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CelesTrak

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  • Name(s): Top 25 by Relative Speed
  • Order by Relative Speed
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Data current as of 2026 Feb 15 14:05:50 UTC

Computation Interval: Start = 2026 Feb 15 15:00:00 UTC, Stop = 2026 Feb 22 15:00:00 UTC
Computation Threshold: 5.0 km
Considering: 14,388 Primaries, 29,959 Secondaries (114,012 Conjunctions)
21 SGP4 Propagation Errors
Computation run time: 08h 52m 37.876s

SOCRATES Format Documentation

See notes at bottom of page for data field descriptions

Data
&
Graphs
NORAD
Catalog
Number
Name [Ops Status] Days
Since
Epoch
TCA
(UTC)
Min
Range
(km)
Relative
Speed
(km/sec)
Max
Probability
Dilution
Threshold
(km)
GP Data 28413 SHIJIAN-6 01A (SJ-6 01A) [+] 5.505 2026-02-20 13:56:47.878 4.064 17.133
50 km All 27883 COSMOS 917 DEB [-] 5.942 1.082E-07 2.367
GP Data 67590 STARLINK-36376 [+] 0.408 2026-02-15 15:47:38.352 3.018 17.118
50 km All 19535 SL-12 R/B(AUX MOTOR) [-] 0.662 5.071E-06 1.930
GP Data 59134 JACKAL X-1L-002 [+] 3.797 2026-02-18 17:25:34.111 2.232 16.996
50 km All 16446 SL-12 R/B(AUX MOTOR) [-] 3.623 2.219E-07 1.441
GP Data 57200 OBJECT AL [+] 6.797 2026-02-22 01:39:23.933 3.615 16.954
50 km All 18374 SL-12 R/B(AUX MOTOR) [-] 7.291 8.556E-08 2.303
GP Data 65456 STARLINK-35005 [+] 4.049 2026-02-19 05:16:16.467 4.530 16.832
50 km All 29680 SL-12 R/B(AUX MOTOR) [-] 4.874 2.407E-06 2.886
GP Data 65521 STARLINK-35187 [+] 0.636 2026-02-15 19:16:43.153 4.014 16.784
50 km All 48541 SL-12 DEB [-] 2.044 3.094E-06 2.534
GP Data 55638 STARLINK-5507 [+] 4.463 2026-02-19 11:36:30.878 4.333 16.604
50 km All 12624 DYNAMICS EXPLORER 1 [?] 6.483 5.761E-06 2.454
GP Data 60575 HAWK-10C [+] 2.767 2026-02-17 23:03:28.570 4.374 16.557
50 km All 20630 SL-12 R/B(AUX MOTOR) [-] 3.712 6.365E-08 2.562
GP Data 56491 STARLINK-5842 [+] 5.503 2026-02-20 05:38:30.433 3.298 16.466
50 km All 3174 OV1-14 [?] 5.591 4.124E-06 2.251
GP Data 52159 ENMAP [+] 5.776 2026-02-21 00:50:17.261 3.922 16.418
50 km All 23402 SL-12 R/B(AUX MOTOR) [-] 5.887 8.070E-08 2.251
Data
&
Graphs
NORAD
Catalog
Number
Name [Ops Status] Days
Since
Epoch
TCA
(UTC)
Min
Range
(km)
Relative
Speed
(km/sec)
Max
Probability
Dilution
Threshold
(km)
GP Data 64886 OBJECT L [+] 7.231 2026-02-22 11:33:57.651 2.474 16.238
50 km All 23811 TITAN 34B AGENA D DEB [-] 7.885 3.076E-07 1.367
GP Data 57696 JILIN-1 KUANFU 02A [+] 0.706 2026-02-15 22:23:00.108 1.312 16.205
50 km All 23292 SL-12 DEB [-] 1.094 1.139E-06 0.696
GP Data 67433 YAOGAN-50 01 [+] 7.373 2026-02-22 14:49:33.385 4.645 16.163
50 km All 55972 FALCON 9 R/B [-] 7.846 8.021E-08 2.793
GP Data 41925 IRIDIUM 112 [+] 7.002 2026-02-22 05:59:21.880 3.730 16.141
50 km All 3174 OV1-14 [?] 7.606 9.493E-08 2.509
GP Data 53545 STARLINK-4475 [+] 1.621 2026-02-16 22:21:49.602 2.165 16.128
50 km All 3177 OV1-14 R/B [-] 2.139 1.139E-05 1.277
GP Data 65064 STARLINK-34793 [+] 5.538 2026-02-20 16:54:34.289 3.829 16.045
50 km All 29323 SL-12 DEB [-] 6.965 4.061E-06 2.024
GP Data 61738 SITRO-AIS 15 [+] 1.722 2026-02-16 23:11:45.585 4.210 15.955
50 km All 2367 WESTFORD NEEDLES [-] 1.757 8.979E-08 2.749
GP Data 61789 SITRO-AIS 17 [+] 1.120 2026-02-16 09:51:57.350 4.508 15.949
50 km All 2367 WESTFORD NEEDLES [-] 1.202 7.863E-08 2.935
GP Data 60013 OBJECT B [+] 0.556 2026-02-15 20:39:56.476 2.332 15.854
50 km All 29008 ELEKTRON 3 DEB [-] 13.768 3.125E-07 1.428
GP Data 62649 AE1C [+] 7.227 2026-02-22 09:57:20.443 1.534 15.828
50 km All 21819 INTERCOSMOS 25 [?] 7.214 1.868E-05 1.084
Data
&
Graphs
NORAD
Catalog
Number
Name [Ops Status] Days
Since
Epoch
TCA
(UTC)
Min
Range
(km)
Relative
Speed
(km/sec)
Max
Probability
Dilution
Threshold
(km)
GP Data 51469 STARLINK-3182 [+] 0.794 2026-02-16 00:49:58.630 3.672 15.812
50 km All 3825 OV1-19 [?] 0.989 3.665E-06 2.275
GP Data 67218 STARLINK-36211 [+] 6.937 2026-02-22 04:29:52.449 2.391 15.775
50 km All 2622 OV1-9 R/B [-] 7.309 8.262E-06 1.594
GP Data 65389 STARLINK-34993 [+] 6.741 2026-02-21 22:40:57.287 4.546 15.707
50 km All 24285 FAST [-] 6.691 2.267E-06 3.188
GP Data 55987 STARLINK-5915 [+] 5.153 2026-02-19 22:32:06.725 4.036 15.697
50 km All 3177 OV1-14 R/B [-] 5.147 3.682E-06 2.118
GP Data 54251 JILIN-1 GAOFEN 03D08 [+] 5.622 2026-02-20 22:11:03.461 4.516 15.691
50 km All 24286 PEGASUS R/B [-] 5.937 1.028E-07 2.874

25 records found

Data Fields:
  • Data: The GP Data button links to a page which provides the GP data used to generate the associated prediction.
  • NORAD Catalog Number: NORAD Catalog Numbers of the two conjuncting objects.
  • Name: SATCAT names of the two conjuncting objects. Operational status of each object is shown in brackets, using the standard CelesTrak SATCAT codes.
  • Days Since Epoch: The number of days from the epoch of the NORAD GP or SupGP (green) element set used to produce the prediction until the time of closest approach for the conjunction.
  • TCA (UTC): Time of closest approach.
  • Min Range (km): The distance between the two conjuncting objects at the time of closest approach.
  • Relative Speed (km/sec): Relative speed of the two conjuncting objects at the time of closest approach.
  • Max Probability: Given fixed spherical object radii and relative distance at the time of closest approach (TCA), the projected covariance ellipse is sized and oriented to produce the maximum probability. For these reports the ratio of major-to-minor axes of the projected covariance ellipse is set using radial, in-track, and cross-track values of 100 m, 300 m, 100 m, respectively. If the combined object radius is greater than the relative distance, the maximum probability will be one; such occurrences are not addressed here. For more details on the maximum probability method, see Dr. Sal Alfano's paper titled "Relating Position Uncertainty to Maximum Conjunction Probability".
  • Dilution Threshold (km): The standard deviation that produces the maximum probability defines the threshold of dilution. A smaller or larger standard deviation will produce a smaller probability. In the case of computing true probability with a smaller standard deviation, the data is of sufficient quality to associate low probability with low risk. For a larger standard deviation, this is not the case and the resulting true probability calculation becomes "diluted." If operating in this dilution region, the recommendation is to obtain better data and reassess the encounter. If time or resources do not permit, then the maximum probability should be used in place of the true probability.
  • SGP4 Propagation Errors: A list of objects which were not screened because their GP data shows they have already decayed (but haven't yet been reflected in the SATCAT) or will decay prior to the end of the computation interval.