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CelesTrak

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  • Name(s): Top 10 by Relative Speed
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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 39440 CUBEBUG-2 (LO-74) [+] 1.720 2024-12-10 13:26:12.140 4.708 16.698
50 km All 41700 SL-12 DEB [-] 1.933 7.396E-08 2.988
GP Data 43075 IRIDIUM 134 [+] 2.318 2024-12-10 16:02:41.083 0.557 16.510
50 km All 14621 DELTA 1 DEB [-] 1.863 5.518E-06 0.339
GP Data 60472 CONNECTA IOT-1 [+] 4.849 2024-12-14 00:30:53.694 4.509 16.487
50 km All 33472 SL-12 R/B(AUX MOTOR) [-] 5.900 9.077E-08 2.539
GP Data 61903 OBJECT K [+] 5.324 2024-12-14 11:25:10.985 3.960 16.438
50 km All 33472 SL-12 R/B(AUX MOTOR) [-] 6.355 1.192E-07 2.205
GP Data 55047 NUSAT-33 (ALBANIA-2) [+] 3.532 2024-12-12 15:28:11.717 2.277 16.430
50 km All 15714 SL-12 R/B(AUX MOTOR) [-] 4.035 2.461E-07 1.273
GP Data 46503 LEMUR-2-NICHOL [+] 4.351 2024-12-13 07:13:33.006 0.154 16.367
50 km All 44867 CZ-3B R/B [-] 4.569 8.095E-05 0.083
GP Data 57861 VICTUS NOX [+] 6.015 2024-12-15 02:28:54.785 4.592 16.360
50 km All 37828 BREEZE-M DEB [-] 6.620 9.510E-08 2.380
GP Data 40119 BRITE-PL2 (HEWELIUSZ) [+] 4.029 2024-12-12 20:59:43.336 1.746 16.337
50 km All 61188 OBJECT D [-] 3.760 6.027E-07 0.989
GP Data 51880 STARLINK-3566 [+] 4.467 2024-12-13 12:53:31.448 4.833 16.294
50 km All 24911 DELTA 1 DEB [-] 5.386 2.626E-06 2.480
GP Data 55019 KSF3-B [+] 6.376 2024-12-15 12:39:09.306 4.888 16.278
50 km All 37187 BREEZE-M DEB [-] 7.367 7.985E-08 2.666

10 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.