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Search parameters:

  • NORAD Catalog Number(s): 25544
  • Order by Minimum Range
  • Return first 25 items

Data current as of 2023 Sep 22 08:06:19 UTC

Computation Interval: Start = 2023 Sep 22 08:00:00 UTC, Stop = 2023 Sep 29 08:00:00 UTC
Computation Threshold: 5.0 km
Considering: 8,617 Primaries, 25,633 Secondaries (67,904 Conjunctions)
9 SGP4 Propagation Errors
Computation run time: 04h 54m 07.926s

SOCRATES Format Documentation

See notes at bottom of page for data field descriptions

Name [Ops Status] Days
GP Data 25544 ISS (ZARYA) [+] 4.905 2023-09-27 02:05:44.286 1.730 14.659
50 km All 43133 CNUSAIL-1 [+] 4.910 3.862E-05 0.944
GP Data 25544 ISS (ZARYA) [+] 5.224 2023-09-27 09:44:45.736 1.853 14.375
50 km All 47457 LEMUR-2-NALLYWACKER [+] 5.495 3.646E-05 0.934
GP Data 25544 ISS (ZARYA) [+] 5.893 2023-09-28 01:49:05.535 3.156 9.981
50 km All 43855 CHOMPTT [+] 6.075 2.119E-05 0.943
GP Data 25544 ISS (ZARYA) [+] 1.449 2023-09-23 15:09:30.422 3.442 14.030
50 km All 48250 OBJECT C [-] 1.460 1.136E-05 1.615
GP Data 25544 ISS (ZARYA) [+] 5.127 2023-09-27 07:25:22.366 3.903 14.331
50 km All 47457 LEMUR-2-NALLYWACKER [+] 5.398 8.250E-06 1.960
GP Data 25544 ISS (ZARYA) [+] 0.384 2023-09-22 13:36:26.896 4.729 11.627
50 km All 34445 COSMOS 2251 DEB [-] 0.587 8.366E-06 1.595

6 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.