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CelesTrak

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  • Name(s): Top 10 by Relative Speed
  • Order by Relative Speed
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Data current as of 2025 Apr 21 08:07:44 UTC

Computation Interval: Start = 2025 Apr 21 08:00:00 UTC, Stop = 2025 Apr 28 08:00:00 UTC
Computation Threshold: 5.0 km
Considering: 11,303 Primaries, 27,288 Secondaries (80,179 Conjunctions)
12 SGP4 Propagation Errors
Computation run time: 06h 07m 22.833s

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 57169 OBJECT D [+] 4.153 2025-04-25 08:10:13.118 3.371 16.839
50 km All 41681 SL-12 DEB [-] 9.063 1.439E-07 2.145
GP Data 37765 SJ-11-02 [+] 5.953 2025-04-27 05:06:56.739 4.190 16.667
50 km All 19856 SL-12 R/B(AUX MOTOR) [-] 6.823 6.404E-08 2.658
GP Data 55053 EOSSAT-1 [+] 1.800 2025-04-22 11:59:44.795 3.804 16.661
50 km All 22671 MOLNIYA 1-86 [?] 1.597 3.313E-07 2.405
GP Data 50572 TIANHUI 4A [+] 3.742 2025-04-24 23:11:01.596 3.119 16.634
50 km All 42974 SL-12 DEB [-] 4.388 1.877E-07 1.777
GP Data 54692 JILIN-1 GAOFEN 03D47 [+] 6.399 2025-04-27 13:38:12.365 4.813 16.426
50 km All 84188 UNKNOWN [-] 8.572 7.135E-08 3.030
GP Data 52764 NUSAT-29 (EDITH CLARKE) [+] 0.903 2025-04-22 02:26:06.545 4.931 16.413
50 km All 31103 BREEZE-M DEB [-] 1.964 7.853E-08 2.687
GP Data 49422 STARLINK-3161 [+] 4.937 2025-04-25 16:16:14.777 3.554 16.395
50 km All 12624 DYNAMICS EXPLORER 1 [?] 4.817 9.200E-06 1.873
GP Data 60572 OBJECT DJ [+] 1.066 2025-04-22 07:03:48.967 3.452 16.311
50 km All 29325 SL-12 DEB [-] 1.120 1.615E-07 1.867
GP Data 60509 FLOCK 4BE-29 [+] 7.067 2025-04-27 17:06:32.440 4.259 16.295
50 km All 34230 BREEZE-M DEB [-] 17.634 1.034E-07 2.359
GP Data 58435 COSMOS 2572 [+] 2.325 2025-04-23 03:31:11.839 4.234 16.233
50 km All 38601 BREEZE-M DEB [-] 6.009 1.141E-07 2.155

10 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.