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CelesTrak

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  • Name(s): Top 25 by Minimum Range
  • Order by Minimum Range
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Data current as of 2025 Dec 09 20:05:47 UTC

Computation Interval: Start = 2025 Dec 09 19:00:00 UTC, Stop = 2025 Dec 16 19:00:00 UTC
Computation Threshold: 5.0 km
Considering: 13,576 Primaries, 29,159 Secondaries (105,499 Conjunctions)
20 SGP4 Propagation Errors
Computation run time: 08h 44m 37.566s

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 52682 STARLINK-4017 [+] 1.657 2025-12-10 22:15:40.010 0.009 2.744
50 km All 11114 SL-8 DEB [-] 1.922 1.000E+00 0.000
GP Data 47856 YAOGAN-31 04B [+] 5.947 2025-12-15 13:52:13.690 0.013 14.155
50 km All 25569 SL-8 R/B [-] 6.188 5.322E-02 0.007
GP Data 54099 STARLINK-5198 [+] 6.453 2025-12-15 21:05:38.359 0.014 14.634
50 km All 31330 FENGYUN 1C DEB [-] 6.872 2.648E-01 0.007
GP Data 46809 YAOGAN-30 08C [+] 2.315 2025-12-11 23:01:59.144 0.017 5.676
50 km All 58510 STARLINK-30989 [+] 2.569 2.626E-01 0.005
GP Data 54677 ONEWEB-0655 [+] 4.670 2025-12-14 04:49:58.730 0.022 9.475
50 km All 29168 SCOUT B DEB [-] 5.129 2.300E-02 0.007
GP Data 64055 QPS-SAR-10 (WADATSUMI-I) [+] 2.047 2025-12-11 05:32:06.557 0.032 6.648
50 km All 26086 DUMSAT [?] 1.646 3.823E-03 0.008
GP Data 29506 SHIJIAN-6 02B (SJ-6 02B) [+] 3.798 2025-12-13 10:02:10.823 0.038 14.160
50 km All 58480 STARLINK-30984 [+] 4.093 4.203E-02 0.019
GP Data 58980 STARLINK-31353 [+] 4.908 2025-12-14 05:09:39.244 0.040 14.412
50 km All 43682 H-2A R/B [-] 4.712 3.656E-02 0.021
GP Data 63735 KUIPER-00020 [+] 4.058 2025-12-13 11:46:07.119 0.041 14.456
50 km All 31132 CP4 [-] 4.056 1.144E-03 0.022
GP Data 64296 STARLINK-34443 [+] 3.544 2025-12-13 00:08:36.213 0.045 4.373
50 km All 54523 CZ-6A DEB [-] 3.840 5.860E-02 0.011
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 54045 YAOGAN-36 02C [+] 2.314 2025-12-11 09:31:02.230 0.049 8.737
50 km All 66464 STARLINK-35435 [+] 1.813 1.554E-03 0.014
GP Data 59406 STARLINK-31391 [+] 6.396 2025-12-15 10:13:25.813 0.050 9.408
50 km All 59778 OBJECT F [+] 6.078 4.101E-02 0.015
GP Data 5398 RIGIDSPHERE 2 (LCS 4) [+] 2.318 2025-12-11 22:09:57.093 0.051 14.750
50 km All 41258 NOAA 16 DEB [-] 3.994 6.349E-04 0.032
GP Data 42807 IRIDIUM 118 [+] 1.903 2025-12-11 05:40:53.382 0.051 10.062
50 km All 37404 FENGYUN 1C DEB [-] 1.971 1.286E-03 0.016
GP Data 53556 STARLINK-4505 [+] 4.929 2025-12-14 13:26:27.616 0.051 6.644
50 km All 54911 CZ-6A DEB [-] 5.410 4.368E-02 0.013
GP Data 42954 VRSS-2 [+] 2.582 2025-12-12 04:31:05.856 0.052 12.194
50 km All 32221 FENGYUN 1C DEB [-] 3.518 1.073E-03 0.019
GP Data 62626 MBZ-SAT [+] 0.166 2025-12-09 19:18:03.421 0.053 6.699
50 km All 66296 BANDWAGON-4D [+] 2.074 1.430E-03 0.014
GP Data 49766 STARLINK-3190 [+] 5.667 2025-12-14 23:17:03.946 0.055 12.826
50 km All 18490 COSMOS 252 DEB [-] 5.887 2.649E-02 0.021
GP Data 56153 PIESAT A [+] 3.412 2025-12-12 23:38:39.994 0.056 0.001
50 km All 56156 PIESAT D [+] 3.412 1.405E-03 0.013
GP Data 56153 PIESAT A [+] 3.478 2025-12-13 01:13:52.029 0.059 0.001
50 km All 56156 PIESAT D [+] 3.478 1.405E-03 0.013
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 48010 STARLINK-2226 [+] 3.310 2025-12-12 16:46:40.865 0.061 14.420
50 km All 63347 YUNYAO-1 46 [+] 3.088 1.580E-02 0.032
GP Data 59337 STARLINK-31612 [+] 2.742 2025-12-12 00:47:41.240 0.063 5.956
50 km All 34693 IRIDIUM 33 DEB [-] 2.390 2.956E-02 0.016
GP Data 55273 STARLINK-5291 [+] 2.720 2025-12-12 05:51:50.779 0.064 7.013
50 km All 24213 PEGASUS DEB [-] 2.845 2.784E-02 0.017
GP Data 60279 STARLINK-32010 [+] 2.969 2025-12-12 01:08:39.086 0.066 10.352
50 km All 60458 YAOGAN-43 01A [+] 2.811 2.299E-02 0.020
GP Data 60539 ICEYE-X43 [+] 6.470 2025-12-15 23:01:34.613 0.067 4.506
50 km All 63873 STARLINK-33987 [+] 6.468 2.758E-02 0.017

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.