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CelesTrak

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  • Name(s): Top 25 by Time of Closest Approach
  • Order by Time of Closest Approach
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Data current as of 2025 Apr 21 08:07:44 UTC

Computation Interval: Start = 2025 Apr 21 08:00:00 UTC, Stop = 2025 Apr 28 08:00:00 UTC
Computation Threshold: 5.0 km
Considering: 11,303 Primaries, 27,288 Secondaries (80,179 Conjunctions)
12 SGP4 Propagation Errors
Computation run time: 06h 07m 22.833s

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 48787 ONEWEB-0210 [+] 0.756 2025-04-21 08:00:09.377 1.055 14.550
50 km All 4929 THORAD AGENA D DEB [-] 1.219 4.376E-06 0.730
GP Data 33499 KKS-1 (KISEKI) [+] 0.451 2025-04-21 08:00:13.423 2.800 14.880
50 km All 35594 COSMOS 2251 DEB [-] 4.580 2.060E-07 1.804
GP Data 43111 CARTOSAT-2F [+] 0.181 2025-04-21 08:00:25.725 3.157 0.183
50 km All 43803 JY1SAT (JO-97) [+] 0.181 4.429E-07 0.744
GP Data 56747 OBJECT E [+] 0.168 2025-04-21 08:00:27.265 3.098 12.910
50 km All 22315 IUS R/B(1) [-] 0.732 9.415E-07 1.024
GP Data 45219 STARLINK-1187 [P] 0.084 2025-04-21 08:00:28.250 0.828 11.056
50 km All 63188 STARLINK-11642 [+] 0.954 4.745E-04 0.265
GP Data 51963 STARLINK-3675 [+] 1.397 2025-04-21 08:00:32.807 4.425 10.877
50 km All 58578 QPS-SAR-5 (TSUKUYOMI-I) [+] 0.492 5.028E-06 1.415
GP Data 48693 STARLINK-2618 [+] 0.116 2025-04-21 08:00:37.087 4.754 11.637
50 km All 61894 OBJECT A [+] 0.109 4.074E-06 1.625
GP Data 52908 YAOGAN-35 02B [+] 0.475 2025-04-21 08:00:38.628 4.541 4.216
50 km All 62496 STARLINK-32718 [+] 0.730 6.253E-06 1.109
GP Data 44925 STARLINK-1112 [+] 0.414 2025-04-21 08:00:45.403 3.285 11.412
50 km All 63357 OTC P1 G [+] 0.407 8.725E-06 1.098
GP Data 37930 CHUANGXIN 1-03 (CX-1-03) [+] 0.149 2025-04-21 08:00:59.419 4.960 14.674
50 km All 61272 CZ-6A DEB [-] 0.789 6.706E-08 3.128
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 46912 KSM1-A [+] 0.142 2025-04-21 08:01:05.230 1.133 9.439
50 km All 48273 LEMUR-2-SPECIAL-K [+] 0.137 2.790E-06 0.329
GP Data 45776 STARLINK-1489 [P] 0.085 2025-04-21 08:01:47.788 2.908 1.468
50 km All 62916 STARLINK-11430 [+] 0.863 5.199E-05 0.688
GP Data 57431 STARLINK-30170 [P] 0.085 2025-04-21 08:01:52.239 3.409 2.979
50 km All 62288 STARLINK-33565 [+] 0.533 3.734E-05 0.817
GP Data 25415 ORBCOMM FM19 [+] 0.403 2025-04-21 08:02:13.783 4.479 13.419
50 km All 25078 IRIDIUM 44 [-] 0.872 1.563E-06 1.983
GP Data 53611 STARLINK-4650 [P] 0.418 2025-04-21 08:02:19.645 2.704 5.774
50 km All 58269 IRIS-C2 [+] 0.129 1.707E-05 0.682
GP Data 41899 YIJIAN [+] 0.471 2025-04-21 08:02:19.670 4.716 14.675
50 km All 2125 OPS 0340 [?] 0.453 7.589E-08 2.907
GP Data 60393 QIANFAN-15 [+] 0.187 2025-04-21 08:02:21.212 2.251 9.947
50 km All 40817 CZ-3C DEB [-] 4.744 7.246E-07 0.638
GP Data 55031 FLOCK 4Y-17 [+] 0.679 2025-04-21 08:02:30.353 3.803 13.541
50 km All 56754 TROPICS-07 [+] 0.185 8.288E-08 1.616
GP Data 55471 STARLINK-5711 [+] 0.816 2025-04-21 08:02:32.955 2.857 10.974
50 km All 32314 FENGYUN 1C DEB [-] 4.845 1.200E-05 0.918
GP Data 47408 STARLINK-2135 [+] 0.237 2025-04-21 08:02:40.192 4.489 12.763
50 km All 407 THOR ABLESTAR DEB [-] 0.845 4.035E-06 1.738
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 55613 STARLINK-5715 [+] 0.425 2025-04-21 08:02:41.614 2.296 13.997
50 km All 12230 DELTA 1 DEB [-] 0.675 1.253E-05 1.094
GP Data 39419 DUBAISAT-2 [+] 0.140 2025-04-21 08:02:49.470 2.386 14.224
50 km All 53905 STARLINK-5003 [+] 0.355 1.103E-05 1.196
GP Data 49260 LANDSAT 9 [+] 0.181 2025-04-21 08:02:57.601 4.499 14.781
50 km All 4231 THORAD AGENA D DEB [-] 0.610 8.048E-08 2.870
GP Data 58929 COSMOS 2575 [+] 0.281 2025-04-21 08:03:09.397 3.098 15.276
50 km All 58324 FLOCK 4Q-10 [-] 0.131 1.639E-07 2.050
GP Data 44358 FORMOSAT 7-5 [+] 0.551 2025-04-21 08:03:09.567 3.993 10.332
50 km All 58025 PVCC [+] 0.162 2.126E-07 1.226

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.