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SJ-6C

In orbit NORAD 29505 QGLR-3538-1926-9702-3703 China

2006

Launch

0

Observations all time

Mission information
Spacecraft name
SJ-6C
Other names
2006-046A
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
2006-10-23 00:00:00
Separation time
2006-10-23 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
505.62 km
Apogee
512.06 km
Inclination
97.6°
Period
94.9 min
Semi-major axis
6886.9 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 29505U 06046A   26283.61707162  .00007060  00000-0  35032-3 0  9997
2 29505 97.6244 325.5695 0004627 97.1344 263.0415 15.18016667 89770
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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 00:10:29 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
PEGASUS DEB
NORAD 24007
1.028 15.22 1.4e-06
2026-10-12 05:12:08 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
OPTISAT
NORAD 68418
3.730 10.17 2.5e-07
2026-10-12 17:01:54 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
YAM-9
NORAD 66694
1.643 3.61 1.6e-06
2026-10-15 02:46:26 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
AC1-001
NORAD 66744
1.709 3.78 1.5e-06
2026-10-15 07:39:33 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
SBSS (USA 216)
NORAD 37168
4.754 14.71 8.1e-08
2026-10-15 09:14:29 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
SBSS (USA 216)
NORAD 37168
2.282 14.71 3.5e-07
2026-10-15 14:15:51 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
XIWANG-5 02
NORAD 67069
4.762 14.25 9.1e-08
2026-10-15 18:43:03 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
COSMOS 2251 DEB
NORAD 33811
4.516 6.85 2.0e-07
2026-10-15 20:17:59 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
COSMOS 2251 DEB
NORAD 33811
2.095 6.83 9.1e-07
2026-10-16 05:01:02 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
SBSS (USA 216)
NORAD 37168
4.733 14.67 8.1e-08
2026-10-16 14:29:54 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
COSMOS 2251 DEB
NORAD 33811
1.746 6.56 1.3e-06
2026-10-16 16:04:51 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
COSMOS 2251 DEB
NORAD 33811
3.686 6.54 3.0e-07
2026-10-16 22:17:29 SHIJIAN-6 02A (SJ-6 02A)
NORAD 29505
RASSVET-3 22
NORAD 100088
1.817 15.01 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