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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 Feb 14 08:05:55 UTC

Computation Interval: Start = 2025 Feb 14 08:00:00 UTC, Stop = 2025 Feb 21 08:00:00 UTC
Computation Threshold: 5.0 km
Considering: 11,024 Primaries, 27,142 Secondaries (80,823 Conjunctions)
18 SGP4 Propagation Errors
Computation run time: 06h 19m 11.202s

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 39268 POPACS 1 [+] 0.843 2025-02-14 14:38:03.971 0.015 9.378
50 km All 38763 CP5 [-] 0.909 1.564E-02 0.004
GP Data 57022 OBJECT U [+] 2.658 2025-02-16 14:27:32.916 0.020 13.950
50 km All 59869 STARLINK-31760 [+] 2.504 1.581E-01 0.009
GP Data 47558 STARLINK-1957 [+] 7.327 2025-02-21 05:50:11.643 0.023 8.086
50 km All 30194 FENGYUN 1C DEB [-] 7.271 1.671E-01 0.007
GP Data 38771 METOP-B [+] 3.857 2025-02-18 00:37:52.138 0.024 13.545
50 km All 34019 COSMOS 2251 DEB [-] 4.080 3.908E-03 0.011
GP Data 60472 CONNECTA IOT-1 [+] 4.231 2025-02-18 09:46:19.099 0.024 15.106
50 km All 60965 CZ-6A DEB [-] 4.210 2.707E-03 0.016
GP Data 44387 METEOR-M2 2 [P] 1.105 2025-02-15 05:50:01.417 0.030 10.893
50 km All 42429 NOAA 16 DEB [-] 1.597 3.475E-03 0.010
GP Data 44934 STARLINK-1071 [+] 1.505 2025-02-14 20:46:33.789 0.031 4.221
50 km All 22433 SL-16 DEB [-] 0.776 1.120E-01 0.008
GP Data 59066 SITRO-AIS 25 [+] 2.702 2025-02-16 20:44:29.917 0.034 14.963
50 km All 24126 PEGASUS DEB [-] 3.347 1.301E-03 0.024
GP Data 57629 HEAD-3D [+] 1.156 2025-02-15 05:29:17.450 0.046 13.557
50 km All 60783 CZ-6A DEB [-] 1.482 1.112E-03 0.020
GP Data 54150 GONETS-M 23 [+] 1.096 2025-02-15 05:16:26.277 0.048 13.746
50 km All 21108 SL-8 R/B [-] 1.053 3.919E-03 0.027
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 62459 SDX01 [+] 0.187 2025-02-14 08:59:37.688 0.049 0.000
50 km All 62460 SDX02 [+] 0.513 1.816E-03 0.012
GP Data 58340 LEMUR-2-MJR092620 [+] 4.473 2025-02-18 15:53:38.741 0.053 14.740
50 km All 60143 STARLINK-32027 [+] 4.509 1.928E-02 0.030
GP Data 49766 STARLINK-3190 [+] 0.938 2025-02-14 10:23:20.915 0.054 4.386
50 km All 33890 COSMOS 2251 DEB [-] 0.207 4.055E-02 0.014
GP Data 56798 STARLINK-6068 [+] 4.891 2025-02-18 19:47:23.365 0.059 8.873
50 km All 31355 FENGYUN 1C DEB [-] 5.069 3.071E-02 0.017
GP Data 43927 IRIDIUM 172 [+] 5.641 2025-02-19 12:16:44.051 0.060 14.861
50 km All 270305 UNKNOWN [-] 6.666 4.134E-04 0.042
GP Data 56153 PIESAT A [+] 0.823 2025-02-14 09:18:26.946 0.060 0.000
50 km All 56154 PIESAT B [+] 0.823 1.220E-03 0.014
GP Data 45726 ANDESITE [+] 1.407 2025-02-15 04:22:01.719 0.062 11.127
50 km All 56384 STARLINK-6153 [+] 1.544 2.407E-02 0.020
GP Data 54227 MATS [+] 1.654 2025-02-15 14:06:46.641 0.062 11.187
50 km All 55760 STARLINK-5532 [+] 2.054 2.450E-02 0.020
GP Data 62630 OBJECT X [+] 3.341 2025-02-17 01:17:14.346 0.062 0.002
50 km All 62664 OBJECT BH [+] 2.946 1.144E-03 0.015
GP Data 59911 TIANQI 27 [+] 5.227 2025-02-19 07:48:09.025 0.066 9.786
50 km All 37670 DELTA 1 DEB [-] 9.746 7.839E-04 0.020
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 54168 STARLINK-5245 [+] 6.168 2025-02-20 06:37:22.646 0.067 14.390
50 km All 58301 IMPULSE-1 MIRA [+] 6.801 1.344E-02 0.035
GP Data 42840 LEMUR-2-FURIAUS [+] 4.589 2025-02-18 14:21:42.396 0.068 9.206
50 km All 54789 STARLINK-5446 [+] 4.525 2.263E-02 0.020
GP Data 48484 STARLINK-2696 [P] 2.070 2025-02-16 06:46:57.613 0.072 6.290
50 km All 58545 STARLINK-31057 [+] 2.796 6.990E-02 0.019
GP Data 45735 STARLINK-1471 [P] 4.892 2025-02-18 14:58:55.436 0.075 10.962
50 km All 60318 STARLINK-32190 [+] 4.677 5.357E-02 0.025
GP Data 58280 FLOCK 4Q-28 [+] 1.187 2025-02-14 20:19:12.441 0.075 13.232
50 km All 58391 STARLINK-30916 [+] 1.260 1.350E-02 0.031

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.