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CelesTrak

Search parameters:

  • Name(s): Top 25 by Maximum Probability
  • Order by Maximum Probability
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Data current as of 2024 Dec 09 08:06:08 UTC

Computation Interval: Start = 2024 Dec 09 08:00:00 UTC, Stop = 2024 Dec 16 08:00:00 UTC
Computation Threshold: 5.0 km
Considering: 10,657 Primaries, 26,899 Secondaries (76,189 Conjunctions)
23 SGP4 Propagation Errors
Computation run time: 06h 07m 08.462s

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 46579 STARLINK-1705 [+] 4.214 2024-12-12 21:17:35.945 0.017 10.205
50 km All 1961 TITAN 3C TRANSTAGE DEB [-] 4.041 2.508E-01 0.005
GP Data 55024 FLOCK 4Y-14 [+] 5.932 2024-12-14 16:15:52.236 0.033 9.957
50 km All 59200 STARLINK-31503 [+] 5.854 7.959E-02 0.010
GP Data 45460 YAOGAN-30 07A [+] 4.875 2024-12-14 00:50:57.342 0.040 5.781
50 km All 49171 STARLINK-3107 [+] 5.547 6.870E-02 0.011
GP Data 62160 STARLINK-32484 [+] 0.737 2024-12-09 21:41:36.309 0.031 14.130
50 km All 43837 OBJECT G [-] 0.720 6.800E-02 0.014
GP Data 43786 ITASAT [+] 2.923 2024-12-11 15:06:48.152 0.048 6.490
50 km All 52699 STARLINK-3987 [+] 2.788 4.832E-02 0.013
GP Data 33412 COSMO-SKYMED 3 [+] 1.888 2024-12-11 00:00:45.575 0.053 8.534
50 km All 55647 STARLINK-5510 [+] 2.089 3.796E-02 0.015
GP Data 57033 OBJECT AF [+] 6.020 2024-12-14 21:46:15.735 0.055 7.051
50 km All 58674 STARLINK-31124 [+] 6.085 3.701E-02 0.015
GP Data 58292 UMBRA-08 [+] 3.989 2024-12-12 18:38:44.972 0.057 10.607
50 km All 59158 STARLINK-31297 [+] 3.848 2.979E-02 0.018
GP Data 53465 STARLINK-4415 [+] 3.907 2024-12-12 23:58:34.217 0.075 6.182
50 km All 20663 COSMOS 2084 [?] 4.171 2.683E-02 0.019
GP Data 59185 STARLINK-31394 [+] 7.372 2024-12-15 21:55:29.910 0.138 2.551
50 km All 59691 STARLINK-32090 [P] 7.311 2.213E-02 0.033
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 53429 STARLINK-4543 [+] 1.542 2024-12-10 07:27:27.647 0.071 11.223
50 km All 34503 IRIDIUM 33 DEB [-] 1.602 1.836E-02 0.024
GP Data 48411 STARLINK-2505 [+] 1.528 2024-12-10 08:31:46.482 0.085 3.890
50 km All 24996 PEGASUS DEB [-] 1.795 1.753E-02 0.021
GP Data 52775 GUARDIAN [+] 0.229 2024-12-09 08:23:41.186 0.082 7.108
50 km All 59670 STARLINK-31860 [+] 0.942 1.737E-02 0.022
GP Data 49138 STARLINK-3058 [+] 7.400 2024-12-15 21:02:11.970 0.063 13.743
50 km All 724 SCOUT X-4 DEB [-] 6.743 1.721E-02 0.029
GP Data 59086 STARLINK-31279 [+] 0.953 2024-12-09 16:47:53.263 0.060 14.232
50 km All 60208 TECHEDSAT-11 [+] 0.850 1.720E-02 0.030
GP Data 55020 FLOCK 4Y-24 [+] 1.389 2024-12-10 06:36:49.024 0.060 14.307
50 km All 59393 STARLINK-31443 [+] 1.503 1.568E-02 0.030
GP Data 56481 STARLINK-6222 [+] 3.778 2024-12-12 18:37:27.572 0.056 15.012
50 km All 61615 OBJECT B [-] 3.662 1.531E-02 0.037
GP Data 56544 STARLINK-6226 [+] 0.974 2024-12-09 19:38:20.907 0.069 13.702
50 km All 54396 CZ-6A DEB [-] 0.725 1.458E-02 0.031
GP Data 57134 STARLINK-6133 [+] 4.720 2024-12-13 16:14:30.915 0.066 14.284
50 km All 61616 OBJECT C [-] 4.565 1.416E-02 0.033
GP Data 57236 STARLINK-6315 [+] 6.025 2024-12-14 17:49:55.197 0.092 7.146
50 km All 61413 CZ-6A DEB [-] 5.746 1.373E-02 0.024
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 60999 STARLINK-11270 [+] 1.672 2024-12-10 05:37:26.228 0.086 11.915
50 km All 31611 FENGYUN 1C DEB [-] 13.471 1.206E-02 0.030
GP Data 59538 STARLINK-31725 [+] 2.427 2024-12-10 23:06:09.034 0.100 7.489
50 km All 54884 CZ-6A DEB [-] 2.442 1.155E-02 0.027
GP Data 43807 EUCROPIS [+] 1.915 2024-12-11 00:58:28.910 0.077 14.251
50 km All 53914 STARLINK-5040 [+] 2.162 1.041E-02 0.039
GP Data 44424 COSMOS 2538 [+] 6.362 2024-12-15 12:07:22.098 0.106 7.802
50 km All 52670 STARLINK-4075 [+] 6.634 1.014E-02 0.029
GP Data 50804 STARLINK-3323 [+] 6.517 2024-12-15 09:48:00.382 0.116 13.910
50 km All 24795 IRIDIUM 5 [-] 6.849 9.214E-03 0.054

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.