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Jumang

In orbit NORAD 53346 WAWX-9857-7939-2112-6410 China

2022

Launch

0

Observations all time

Mission information
Spacecraft name
Jumang
Other names
TECMS
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
2022-08-04 00:00:00
Separation time
2022-08-04 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
497.46 km
Apogee
501.75 km
Inclination
97.3°
Period
94.7 min
Semi-major axis
6877.7 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:37 UTC
Two-line elements (TLE)
1 53346U 22090A   26283.98851021  .00005150  00000-0  23487-3 0  9997
2 53346 97.3019 348.7202 0003114 140.0811 220.0655 15.21058497232416
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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
2026-10-12 10:53:50 TECMS
NORAD 53346
IRIDE-MS1-EAGLET 2-16
NORAD 68452
4.403 12.20 1.5e-07
2026-10-12 12:28:53 TECMS
NORAD 53346
IRIDIUM 33 DEB
NORAD 46971
3.682 15.05 1.2e-07
2026-10-12 14:03:36 TECMS
NORAD 53346
IRIDIUM 33 DEB
NORAD 46971
1.695 15.06 5.6e-07
2026-10-12 14:50:59 TECMS
NORAD 53346
IRIDIUM 33 DEB
NORAD 46971
4.431 15.02 8.1e-08
2026-10-12 19:34:50 TECMS
NORAD 53346
DISCO-2
NORAD 68431
3.628 12.14 2.2e-07
2026-10-12 20:22:12 TECMS
NORAD 53346
DISCO-2
NORAD 68431
2.888 12.17 3.5e-07
2026-10-12 21:09:34 TECMS
NORAD 53346
DISCO-2
NORAD 68431
3.965 12.14 1.8e-07
2026-10-13 08:42:26 TECMS
NORAD 53346
YAOGAN-39 03C
NORAD 57990
2.348 10.33 6.2e-07
2026-10-13 10:42:12 KANOPUS-V 3
NORAD 43180
TECMS
NORAD 53346
4.390 14.92 8.8e-08
2026-10-14 10:19:48 TECMS
NORAD 53346
FENGYUN 1C DEB
NORAD 29771
4.571 14.37 9.6e-08
2026-10-15 02:50:24 TECMS
NORAD 53346
ION SCV-019 (ASTOUNDING ALEXANDRA)
NORAD 68435
1.288 12.14 1.7e-06
2026-10-15 20:14:55 TECMS
NORAD 53346
STARLINK-5920
NORAD 55935
4.727 11.36 4.2e-06
2026-10-16 14:17:21 TECMS
NORAD 53346
CZ-6A DEB
NORAD 56246
4.052 9.23 2.2e-07
2026-10-16 19:53:24 TECMS
NORAD 53346
JIELONG-3 R/B
NORAD 58507
3.071 14.95 1.7e-07
2026-10-16 21:30:42 TECMS
NORAD 53346
STARLINK-5926
NORAD 55944
4.344 11.04 5.2e-06
2026-10-17 01:21:32 TECMS
NORAD 53346
OBJECT AK
NORAD 57037
4.852 5.12 1.8e-07
2026-10-17 09:15:36 TECMS
NORAD 53346
IRIDE-MS1-EAGLET 2-7
NORAD 66701
3.015 0.95 4.8e-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