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SJ-9B

In orbit NORAD 38861 ZETQ-9103-3524-7152-2565 China

2012

Launch

0

Observations all time

Mission information
Spacecraft name
SJ-9B
Other names
2012-056B
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
2012-10-14 00:00:00
Separation time
2012-10-14 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
579.48 km
Apogee
600.05 km
Inclination
97.6°
Period
96.5 min
Semi-major axis
6967.9 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:17 UTC
Two-line elements (TLE)
1 38861U 12056B   26282.76556357  .00001579  00000-0  16223-3 0  9993
2 38861 97.6124 262.8060 0014766 187.8077 172.2914 14.91661868756805
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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
2026-10-11 12:55:22 SJ-9B
NORAD 38861
NOAA 16 DEB
NORAD 41520
2.675 14.95 2.3e-07
2026-10-11 16:58:54 SJ-9B
NORAD 38861
NOAA 16 DEB
NORAD 42374
2.535 14.93 2.5e-07
2026-10-12 02:20:50 SJ-9B
NORAD 38861
CUBY-5
NORAD 69907
4.739 9.74 1.6e-07
2026-10-13 05:24:32 SJ-9B
NORAD 38861
NOAA 16 DEB
NORAD 41348
4.973 14.93 6.5e-08
2026-10-13 07:01:05 SJ-9B
NORAD 38861
NOAA 16 DEB
NORAD 41348
1.031 14.94 1.5e-06
2026-10-13 16:59:08 SJ-9B
NORAD 38861
CUBY-3
NORAD 69875
1.794 9.74 1.1e-06
2026-10-13 19:24:06 SJ-9B
NORAD 38861
CUBY-3
NORAD 69875
2.597 9.77 5.2e-07
2026-10-14 04:24:33 SJ-9B
NORAD 38861
SL-8 DEB
NORAD 15756
4.599 4.67 2.0e-07
2026-10-14 04:36:09 SJ-9B
NORAD 38861
CATCH-1
NORAD 60088
3.240 13.47 2.3e-07
2026-10-14 09:52:13 SJ-9B
NORAD 38861
IO-1
NORAD 68498
2.332 3.06 8.0e-07
2026-10-14 16:19:57 SJ-9B
NORAD 38861
ICEYE-X78
NORAD 68995
0.723 10.11 6.6e-06
2026-10-14 17:06:49 SJ-9B
NORAD 38861
IO-1
NORAD 68498
1.279 3.05 2.6e-06
2026-10-14 23:34:33 SJ-9B
NORAD 38861
ICEYE-X78
NORAD 68995
1.194 10.08 2.4e-06
2026-10-15 06:13:31 SJ-9B
NORAD 38861
FENGYUN 1C DEB
NORAD 30569
2.054 14.86 3.9e-07
2026-10-15 06:47:04 SJ-9B
NORAD 38861
SL-14 R/B
NORAD 12988
2.405 14.77 7.1e-07
2026-10-16 10:09:17 SJ-9B
NORAD 38861
IRIDIUM 33 DEB
NORAD 35488
3.470 12.49 2.3e-07
2026-10-16 16:31:17 SJ-9B
NORAD 38861
FENGYUN 1C DEB
NORAD 37444
4.665 13.59 1.1e-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