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CelesTrak

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  • Name(s): Top 25 by NORAD Catalog Number
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Data current as of 2025 Jun 12 08:07:36 UTC

Computation Interval: Start = 2025 Jun 12 08:00:00 UTC, Stop = 2025 Jun 19 08:00:00 UTC
Computation Threshold: 5.0 km
Considering: 11,799 Primaries, 27,702 Secondaries (89,525 Conjunctions)
13 SGP4 Propagation Errors
Computation run time: 06h 35m 51.226s

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 900 CALSPHERE 1 [+] 1.868 2025-06-13 15:02:19.297 3.155 13.907
50 km All 354 THOR ABLESTAR DEB [-] 3.064 8.128E-08 1.609
GP Data 900 CALSPHERE 1 [+] 4.735 2025-06-16 11:50:35.422 3.630 5.073
50 km All 6707 COSMOS 574 [?] 4.609 3.543E-07 0.905
GP Data 900 CALSPHERE 1 [+] 3.524 2025-06-15 06:47:33.183 2.925 14.620
50 km All 12690 COSMOS 1275 DEB [-] 3.504 7.042E-08 2.005
GP Data 900 CALSPHERE 1 [+] 1.207 2025-06-12 23:11:10.397 4.937 9.722
50 km All 14546 COSMOS 1513 [?] 1.134 3.765E-07 1.488
GP Data 900 CALSPHERE 1 [+] 0.956 2025-06-12 17:08:37.864 4.704 2.611
50 km All 27436 COSMOS 2389 [-] 0.501 2.651E-07 1.125
GP Data 900 CALSPHERE 1 [+] 5.963 2025-06-17 17:19:11.964 4.709 14.460
50 km All 29777 FENGYUN 1C DEB [-] 6.037 2.951E-08 2.972
GP Data 900 CALSPHERE 1 [+] 3.651 2025-06-15 09:50:04.615 4.593 1.543
50 km All 270340 UNKNOWN [-] 7.476 8.263E-08 1.087
GP Data 902 CALSPHERE 2 [+] 5.011 2025-06-16 19:09:47.419 4.413 14.214
50 km All 28096 ATLAS 2AS CENTAUR R/B [-] 4.590 3.621E-08 2.584
GP Data 902 CALSPHERE 2 [+] 3.844 2025-06-15 15:09:24.209 4.983 3.169
50 km All 42619 THORAD DELTA 1 DEB [-] 4.009 6.908E-08 1.200
GP Data 902 CALSPHERE 2 [+] 6.104 2025-06-17 21:23:21.925 3.371 7.663
50 km All 54416 CZ-6A DEB [-] 6.060 1.339E-07 0.915
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 902 CALSPHERE 2 [+] 6.069 2025-06-17 20:32:50.223 0.832 11.956
50 km All 60392 QIANFAN-14 [+] 5.722 1.616E-06 0.307
GP Data 902 CALSPHERE 2 [+] 3.973 2025-06-15 18:13:52.777 2.424 13.143
50 km All 62185 OBJECT A [+] 3.941 1.578E-07 1.080
GP Data 902 CALSPHERE 2 [+] 3.701 2025-06-15 11:42:21.095 4.245 1.019
50 km All 62245 QIANFAN-44 [+] 3.572 9.703E-08 1.001
GP Data 902 CALSPHERE 2 [+] 6.511 2025-06-18 07:09:35.334 3.229 1.043
50 km All 62248 QIANFAN-47 [+] 6.386 1.677E-07 0.763
GP Data 1361 LCS 1 [+] 2.622 2025-06-14 12:10:59.265 2.252 6.891
50 km All 1000 TITAN 3A DEB [-] 2.580 7.578E-07 0.610
GP Data 1512 TEMPSAT 1 [+] 1.309 2025-06-12 23:03:23.511 3.425 13.956
50 km All 12729 COSMOS 1275 DEB [-] 2.320 6.832E-08 1.914
GP Data 1512 TEMPSAT 1 [+] 1.473 2025-06-13 02:59:16.180 4.714 6.870
50 km All 32480 BREEZE-M DEB [-] 2.605 7.690E-08 1.235
GP Data 1512 TEMPSAT 1 [+] 4.413 2025-06-16 01:32:41.459 4.984 14.434
50 km All 45280 SL-14 DEB [-] 4.344 2.668E-08 3.376
GP Data 1512 TEMPSAT 1 [+] 7.614 2025-06-19 06:21:42.654 2.267 14.305
50 km All 45334 SL-14 DEB [-] 10.687 1.378E-07 1.434
GP Data 1512 TEMPSAT 1 [+] 1.631 2025-06-13 06:46:40.858 3.914 14.460
50 km All 46466 SL-14 DEB [-] 10.175 4.219E-08 2.711
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 1512 TEMPSAT 1 [+] 3.792 2025-06-15 10:38:51.051 4.109 13.691
50 km All 47533 YAOGAN-31 02B [+] 3.244 5.110E-08 2.133
GP Data 1512 TEMPSAT 1 [+] 6.596 2025-06-18 05:56:06.072 2.451 13.426
50 km All 61601 ONEWEB-0693 [+] 5.997 1.562E-07 1.169
GP Data 1520 CALSPHERE 4A [+] 2.044 2025-06-14 03:31:08.920 3.586 1.599
50 km All 10492 SL-8 R/B [-] 2.312 1.173E-06 0.850
GP Data 1520 CALSPHERE 4A [+] 3.802 2025-06-15 21:42:45.681 2.533 4.689
50 km All 10575 COSMOS 970 DEB [-] 4.045 2.603E-07 0.626
GP Data 1520 CALSPHERE 4A [+] 0.930 2025-06-13 00:46:16.523 3.212 11.198
50 km All 19228 SL-14 DEB [-] 1.082 1.164E-07 1.105

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.