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OBJECT J - 2022-019

In orbit NORAD 51832 SXYS-2180-8616-7867-1442 China

Observations 13
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2022

Launch

13

Observations all time

Mission information
Spacecraft name
OBJECT J - 2022-019
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2022-02-27 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
494.64 km
Apogee
506.00 km
Inclination
97.3°
Period
94.7 min
Semi-major axis
6878.5 km
Velocity
7.61 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:43 UTC
Two-line elements (TLE)
1 51832U 22019J   26280.92804622  .00000812  00000-0  39850-4 0  9994
2 51832  97.3318 340.7778 0008252 182.8815 177.2375 15.20822399254934
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-13 21:35:31 QB50P1
NORAD 40025 		OBJECT J
NORAD 51832 		3.556 5.16 3.3e-07
2026-10-13 21:36:56 PESSOA
NORAD 100139 		OBJECT J
NORAD 51832 		2.445 11.75 5.1e-07
2026-10-13 23:59:05 PESSOA
NORAD 100139 		OBJECT J
NORAD 51832 		2.390 11.78 5.3e-07
2026-10-14 12:08:59 STARLINK-4478
NORAD 53529 		OBJECT J
NORAD 51832 		4.512 14.70 2.7e-06
2026-10-14 14:59:08 PHOBOS
NORAD 68467 		OBJECT J
NORAD 51832 		4.693 11.77 1.4e-07
2026-10-14 14:59:08 IRIDE-MS1-EAGLET 2-10
NORAD 68451 		OBJECT J
NORAD 51832 		4.451 11.76 1.5e-07
2026-10-14 15:46:32 IRIDE-MS1-EAGLET 2-10
NORAD 68451 		OBJECT J
NORAD 51832 		3.765 11.79 2.1e-07
2026-10-14 19:57:45 YAOGAN-39 01C
NORAD 57731 		OBJECT J
NORAD 51832 		1.591 13.33 9.8e-07
2026-10-15 00:27:36 CAMOES
NORAD 68507 		OBJECT J
NORAD 51832 		2.208 11.75 6.2e-07
2026-10-15 01:15:00 CAMOES
NORAD 68507 		OBJECT J
NORAD 51832 		4.664 11.78 1.4e-07
2026-10-16 00:53:29 SITRO-AIS-57
NORAD 67256 		OBJECT J
NORAD 51832 		2.853 1.74 5.4e-07
2026-10-16 05:46:19 KANOPUS-V 4
NORAD 43181 		OBJECT J
NORAD 51832 		2.847 14.80 2.2e-07
2026-10-16 17:28:11 ALSAT-3B
NORAD 67646 		OBJECT J
NORAD 51832 		2.986 1.75 4.9e-07
2026-10-16 23:49:56 JACK-002
NORAD 68417 		OBJECT J
NORAD 51832 		3.441 11.73 2.6e-07
2026-10-17 01:24:41 JACK-002
NORAD 68417 		OBJECT J
NORAD 51832 		2.738 11.73 4.0e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite