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CelesTrak

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  • Name(s): Top 25 by Minimum Range
  • Order by Minimum Range
  • Return first 25 items


Data current as of 2023 Mar 30 08:19:34 UTC

Computation Interval: Start = 2023 Mar 30 09:00:00 UTC, Stop = 2023 Apr 06 09:00:00 UTC
Computation Threshold: 5.0 km
Considering: 7,450 Primaries, 24,764 Secondaries (55,103 Conjunctions)
23 SGP4 Propagation Errors
Computation run time: 04h 27m 00.116s

SOCRATES Format Documentation

See notes at bottom of page for data field descriptions

Re-sort by: Maximum Probability|Minimum Range|Time of Closest Approach|Relative Speed|NORAD Catalog Number

Data NORAD
Catalog
Number
Name [Ops Status] Days
Since
Epoch
TCA
(UTC)
Min
Range
(km)
Relative
Speed
(km/sec)
Max
Probability
Dilution
Threshold
(km)
55484 STARLINK-5696 [+] 2.118 2023-04-01 07:59:29.345 0.015 6.286
33865 IRIDIUM 33 DEB [-] 2.512 1.702E-02 0.004
53367 OBJECT A [+] 3.731 2023-04-02 20:37:54.635 0.016 13.045
3757 COSMOS 249 DEB [-] 4.042 1.031E-02 0.006
32788 AAUSAT-II [P] 6.741 2023-04-05 04:52:47.655 0.024 14.161
53491 STARLINK-4450 [+] 6.352 3.671E-03 0.012
44944 STARLINK-1108 [+] 5.027 2023-04-03 19:49:45.503 0.031 11.177
31305 PEGASUS R/B [-] 5.107 3.263E-03 0.010
46293 3CAT-5B [+] 4.937 2023-04-03 16:03:41.465 0.038 7.924
48914 ICEYE-X12 [+] 4.784 2.672E-03 0.010
51011 FLOCK 4X-29 [+] 5.167 2023-04-04 01:49:04.760 0.038 0.069
51034 FLOCK 4X-23 [-] 5.364 3.053E-03 0.009
51037 FLOCK 4X-10 [+] 2.187 2023-03-31 22:03:09.719 0.054 15.244
51225 COSMOS 1408 DEB [-] 2.758 4.978E-04 0.038
47461 KEPLER-15 (SUDORMRF) [+] 5.762 2023-04-04 14:43:51.241 0.065 1.457
50997 FLOCK 4X-20 [+] 5.889 1.036E-03 0.015
44528 ZY-1 02D [+] 0.396 2023-03-30 13:41:39.549 0.067 11.095
39647 COSMOS 1867 COOLANT [-] 0.889 7.063E-04 0.022
39423 WNISAT-1 [+] 1.798 2023-03-31 21:12:31.456 0.071 14.673
24778 DMSP 5D-2 F14 DEB [-] 2.202 3.384E-04 0.043
Data NORAD
Catalog
Number
Name [Ops Status] Days
Since
Epoch
TCA
(UTC)
Min
Range
(km)
Relative
Speed
(km/sec)
Max
Probability
Dilution
Threshold
(km)
55041 SKYKRAFT-1 [+] 1.372 2023-03-31 06:26:49.630 0.072 15.183
16262 COSMOS 1703 [?] 1.501 2.830E-04 0.051
43519 XJS B [+] 2.376 2023-04-01 05:46:21.196 0.073 13.345
51074 DELFI-PQ [+] 2.491 4.682E-04 0.030
52175 BDSAT [+] 4.412 2023-04-03 04:37:07.258 0.075 12.777
52947 SLINGSHOT 1 [+] 4.490 4.762E-04 0.029
51771 STARLINK-3614 [+] 6.842 2023-04-05 15:32:23.030 0.078 13.271
30800 FENGYUN 1C DEB [-] 7.340 4.145E-04 0.032
42986 COSMOS 2523 [+] 5.610 2023-04-04 12:19:53.812 0.080 13.782
46912 KSM1-A [+] 5.635 3.603E-04 0.036
46914 KSM1-B [+] 6.952 2023-04-06 00:34:10.384 0.081 7.833
54837 STARLINK-5369 [+] 7.172 5.855E-04 0.022
53227 STARLINK-4366 [+] 4.238 2023-04-02 23:47:07.444 0.081 15.145
51616 COSMOS 1408 DEB [-] 6.533 2.230E-04 0.057
53602 STARLINK-4648 [+] 6.831 2023-04-05 01:32:26.467 0.081 3.889
39690 COSMOS 921 DEB [-] 6.745 6.446E-04 0.020
41727 GAOFEN 3 [+] 0.229 2023-03-30 11:09:34.479 0.082 14.453
35836 COSMOS 2251 DEB [-] 0.776 2.686E-04 0.047
53937 STARLINK-4765 [+] 7.285 2023-04-05 23:13:14.675 0.084 13.563
33981 COSMOS 2251 DEB [-] 7.167 3.371E-04 0.037
Data NORAD
Catalog
Number
Name [Ops Status] Days
Since
Epoch
TCA
(UTC)
Min
Range
(km)
Relative
Speed
(km/sec)
Max
Probability
Dilution
Threshold
(km)
55615 STARLINK-5712 [+] 3.273 2023-04-02 03:09:26.722 0.084 11.827
44807 FLOCK 4P-9 [-] 3.336 4.255E-04 0.029
51840 OBJECT S [+] 3.932 2023-04-03 02:57:36.491 0.086 5.288
52746 GHGSAT-C4 [+] 4.262 5.671E-04 0.021
47227 GONETS-M 20 [+] 2.948 2023-04-01 20:28:04.982 0.088 13.692
8613 COSMOS 797 [?] 3.189 1.742E-04 0.049
47961 3B5GSAT (SATELIOT 1) [+] 5.707 2023-04-04 11:45:07.606 0.088 15.059
55690 HORUS 1 [+] 5.307 2.030E-04 0.058
53481 STARLINK-4302 [+] 3.605 2023-04-02 11:20:07.894 0.091 14.932
39539 FENGYUN 1C DEB [-] 9.417 1.976E-04 0.058

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.