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CelesTrak

Search parameters:

  • Name(s): Top 10 by Time of Closest Approach
  • Order by Time of Closest Approach
  • Return first 10 items


Data current as of 2025 May 17 16:05:30 UTC

Computation Interval: Start = 2025 May 17 16:00:00 UTC, Stop = 2025 May 24 16:00:00 UTC
Computation Threshold: 5.0 km
Considering: 11,570 Primaries, 27,474 Secondaries (83,519 Conjunctions)
20 SGP4 Propagation Errors
Computation run time: 06h 08m 16.161s

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 59787 STARLINK-31870 [+] 0.415 2025-05-17 16:00:02.027 1.831 13.574
50 km All 60525 ORESAT0.5 [+] 0.922 2.167E-05 0.793
GP Data 58903 LEMUR-2-CAEL [+] 0.117 2025-05-17 16:00:14.521 1.838 13.428
50 km All 60468 OBJECT A [+] 0.178 7.232E-07 0.783
GP Data 53897 STARLINK-5035 [+] 0.210 2025-05-17 16:00:31.852 2.479 10.817
50 km All 5042 COSMOS 397 DEB [-] 1.327 1.628E-05 0.780
GP Data 55954 STARLINK-5892 [+] 0.533 2025-05-17 16:00:38.095 2.503 14.381
50 km All 38487 COSMOS 2251 DEB [-] 1.433 9.473E-06 1.327
GP Data 53316 YAOGAN-35 03A [+] 0.277 2025-05-17 16:00:42.394 3.391 5.582
50 km All 62950 STARLINK-32850 [+] 0.270 1.090E-05 0.851
GP Data 47831 STARLINK-2420 [+] 0.434 2025-05-17 16:00:42.558 3.717 14.640
50 km All 42849 CICERO 3 [-] 1.195 4.016E-06 2.109
GP Data 45746 STARLINK-1504 [P] 0.463 2025-05-17 16:00:44.112 3.725 10.634
50 km All 62846 STARLINK-32804 [+] 0.158 2.398E-05 1.165
GP Data 58826 STARLINK-31233 [+] 0.430 2025-05-17 16:00:53.937 4.904 10.321
50 km All 52794 CZ-2C R/B [-] 0.771 4.280E-06 1.500
GP Data 42839 LEMUR-2-MONSON [+] 1.179 2025-05-17 16:00:57.834 2.963 9.707
50 km All 52689 STARLINK-4078 [P] 0.250 1.214E-05 0.875
GP Data 58259 LEMUR-2-BASS [+] 0.957 2025-05-17 16:01:00.147 4.034 13.338
50 km All 61702 STARLINK-32299 [+] 0.509 4.633E-06 1.684

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.