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CelesTrak

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  • Name(s): Top 25 by Time of Closest Approach
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Data current as of 2026 Feb 09 00:05:42 UTC

Computation Interval: Start = 2026 Feb 09 00:00:00 UTC, Stop = 2026 Feb 16 00:00:00 UTC
Computation Threshold: 5.0 km
Considering: 14,368 Primaries, 29,969 Secondaries (113,700 Conjunctions)
13 SGP4 Propagation Errors
Computation run time: 09h 16m 09.083s

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 60014 OBJECT C [+] 0.137 2026-02-09 00:00:06.735 4.834 14.989
50 km All 63253 ICEYE-X48 [+] 0.297 6.776E-08 3.177
GP Data 29506 SHIJIAN-6 02B (SJ-6 02B) [+] 0.102 2026-02-09 00:00:11.503 4.553 14.210
50 km All 58508 STARLINK-31026 [+] 0.994 3.017E-06 2.292
GP Data 53497 STARLINK-4453 [+] 0.183 2026-02-09 00:00:20.857 2.808 14.835
50 km All 21397 OKEAN-3 [?] 0.582 1.400E-05 1.742
GP Data 63792 STARLINK-33916 [+] 0.508 2026-02-09 00:00:21.276 3.100 5.446
50 km All 46411 FREGAT DEB [-] 0.982 1.310E-05 0.775
GP Data 50822 STARLINK-3343 [+] 0.999 2026-02-09 00:00:21.535 1.322 14.592
50 km All 60012 OBJECT A [+] 0.161 3.238E-05 0.735
GP Data 56934 GEISAT PRECURSOR [+] 0.121 2026-02-09 00:00:26.989 2.685 10.862
50 km All 62858 STARLINK-32866 [+] 0.181 1.371E-05 0.855
GP Data 55914 STARLINK-5856 [+] 0.684 2026-02-09 00:00:44.167 4.244 13.378
50 km All 41142 NOAA 16 DEB [-] 3.955 4.100E-06 1.809
GP Data 25560 SWAS [B] 0.174 2026-02-09 00:00:50.231 4.721 11.877
50 km All 53819 STARLINK-4738 [+] 0.520 4.041E-06 1.650
GP Data 62615 TRANSPORTER-12G [+] 0.796 2026-02-09 00:00:50.490 3.198 14.965
50 km All 28809 KIRARI (OICETS) [?] 0.353 1.640E-07 1.984
GP Data 62667 FLOCK 4G-14 [+] 0.799 2026-02-09 00:00:51.954 2.762 14.290
50 km All 4133 THORAD AGENA D DEB [-] 0.739 2.713E-07 1.389
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 67426 STARLINK-36146 [+] 0.167 2026-02-09 00:00:54.163 3.510 13.431
50 km All 61163 CZ-6A DEB [-] 0.884 6.114E-06 1.467
GP Data 61768 OBJECT AK [+] 0.127 2026-02-09 00:00:55.468 4.309 15.195
50 km All 67093 STARLINK-35784 [+] 0.489 2.520E-06 2.898
GP Data 58442 STARLINK-30959 [+] 0.517 2026-02-09 00:01:01.987 4.573 10.732
50 km All 27146 PSLV DEB [-] 0.237 4.754E-06 1.448
GP Data 39474 SMDC ONE 2.3 [+] 0.307 2026-02-09 00:01:08.054 4.600 9.447
50 km All 49321 OBJECT G [-] 0.171 1.699E-07 1.331
GP Data 61895 OBJECT B [+] 0.158 2026-02-09 00:01:14.762 4.079 14.470
50 km All 66633 STARLINK-35948 [+] 1.053 3.601E-06 2.143
GP Data 62240 QIANFAN-39 [+] 0.241 2026-02-09 00:01:14.926 3.382 14.834
50 km All 8981 DELTA 1 DEB [-] 0.557 1.307E-07 2.353
GP Data 37849 SUOMI NPP [+] 0.157 2026-02-09 00:01:37.804 4.247 10.790
50 km All 31371 FENGYUN 1C DEB [-] 0.945 1.789E-07 1.369
GP Data 36596 SJ-12 [+] 0.181 2026-02-09 00:01:41.466 3.782 1.804
50 km All 67401 CONNECTA IOT-14 [+] 0.444 3.067E-07 0.897
GP Data 56483 STARLINK-5868 [+] 0.198 2026-02-09 00:01:45.503 3.402 15.050
50 km All 58651 SHIYAN-24C 02 [+] 0.236 4.033E-06 2.294
GP Data 53408 STARLINK-4491 [+] 0.169 2026-02-09 00:01:58.513 2.177 14.796
50 km All 37056 FENGYUN 1C DEB [-] 2.135 1.148E-05 1.259
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 56934 GEISAT PRECURSOR [+] 0.122 2026-02-09 00:02:10.794 4.604 13.894
50 km All 62304 STARLINK-32597 [+] 0.959 3.218E-06 2.125
GP Data 48120 STARLINK-2460 [+] 0.168 2026-02-09 00:02:19.948 3.989 14.671
50 km All 54531 CZ-6A DEB [-] 1.298 3.475E-06 2.270
GP Data 44314 TIANQI-3 [+] 0.172 2026-02-09 00:02:30.183 3.309 13.959
50 km All 52751 TRANSPORTER-5V [-] 0.124 2.039E-07 1.542
GP Data 49164 STARLINK-3106 [+] 0.137 2026-02-09 00:02:32.157 3.607 15.056
50 km All 59105 PE2_FLT1 (TYVAK-0261) [+] 0.164 3.585E-06 2.434
GP Data 56893 STARLINK-6216 [+] 1.013 2026-02-09 00:02:33.465 3.593 9.335
50 km All 39267 DANDE [-] 0.143 8.439E-06 1.038

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.