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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 27 16:05:29 UTC

Computation Interval: Start = 2025 Apr 27 16:00:00 UTC, Stop = 2025 May 04 16:00:00 UTC
Computation Threshold: 5.0 km
Considering: 11,301 Primaries, 27,272 Secondaries (81,016 Conjunctions)
18 SGP4 Propagation Errors
Computation run time: 06h 07m 56.236s

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 26113 IMAGE [P] 4.737 2025-05-01 04:39:53.506 3.998 17.002
50 km All 31323 FENGYUN 1C DEB [-] 24.887 3.261E-03 2.505
GP Data 60574 GNOMES-5 [+] 3.200 2025-04-30 08:43:20.271 4.264 16.942
50 km All 15741 SL-6 R/B(2) [-] 4.541 2.772E-07 2.413
GP Data 62929 KINEIS-2C [+] 4.929 2025-05-02 02:13:46.069 3.621 16.742
50 km All 36406 SL-12 R/B(AUX MOTOR) [-] 5.435 1.227E-07 2.342
GP Data 52151 PUJIANG 2 (PJ-2) [+] 5.637 2025-05-03 03:31:28.102 1.710 16.415
50 km All 20081 SL-12 R/B(AUX MOTOR) [-] 6.331 4.310E-07 0.968
GP Data 46672 STARLINK-1716 [+] 1.031 2025-04-28 12:17:04.339 3.724 16.374
50 km All 12624 DYNAMICS EXPLORER 1 [?] 1.699 8.404E-06 1.957
GP Data 56970 LEMUR-2-EMBRIONOVIS [+] 5.888 2025-05-02 18:14:17.933 1.974 16.366
50 km All 32036 BREEZE-M DEB [-] 6.532 4.768E-07 1.106
GP Data 42988 SKYSAT-C10 [+] 4.114 2025-05-01 01:24:03.999 2.652 16.356
50 km All 32036 BREEZE-M DEB [-] 4.830 1.489E-07 1.482
GP Data 39086 SARAL [+] 2.156 2025-04-29 16:13:08.659 4.129 16.353
50 km All 32280 SL-12 R/B(AUX MOTOR) [-] 3.282 1.017E-07 2.475
GP Data 53450 DONGPO 03 [+] 0.641 2025-04-28 04:40:58.705 4.951 16.210
50 km All 7688 TITAN 34B R/B [-] 2.034 8.084E-08 2.597
GP Data 57175 CUBEBEL 2 (EU11S) [+] 6.422 2025-05-03 21:46:42.423 3.238 16.178
50 km All 41193 BREEZE-M DEB [-] 7.068 1.849E-07 1.738

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.