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LINGQIAO VIDEO B

In orbit NORAD 40960 KTME-4222-3825-6352-1307 CIOMP China

2015

Launch

0

Observations all time

Mission information
Spacecraft name
LINGQIAO VIDEO B
Other names
Jilin-1 SP-02
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
2015-10-07 04:13:00
Separation time
Satellite appearance
Operator
CIOMP
Data for the last 30 days
Orbital parameters of the satellite
Perigee
623.12 km
Apogee
644.60 km
Inclination
97.7°
Period
97.5 min
Semi-major axis
7012.0 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:33 UTC
Two-line elements (TLE)
1 40960U 15057C   26284.95256375  .00001044  00000-0  15253-3 0  9999
2 40960 97.6691 275.1990 0015339 248.6567 111.3008 14.77628226592691
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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 12:06:32 LINGQIAO VIDEO B
NORAD 40960
YZ-1S DEB
NORAD 49385
0.225 14.64 3.5e-05
2026-10-12 12:09:10 YAOGAN-24
NORAD 40310
LINGQIAO VIDEO B
NORAD 40960
3.182 14.35 1.9e-07
2026-10-12 13:03:51 LINGQIAO VIDEO B
NORAD 40960
SL-8 R/B
NORAD 12139
4.737 14.97 3.3e-07
2026-10-12 18:17:09 LINGQIAO VIDEO B
NORAD 40960
ARIRANG-1 (KOMPSAT-1)
NORAD 26032
3.707 14.91 1.2e-07
2026-10-12 19:05:58 LINGQIAO VIDEO B
NORAD 40960
ARIRANG-1 (KOMPSAT-1)
NORAD 26032
4.751 14.92 7.0e-08
2026-10-12 19:54:42 LINGQIAO VIDEO B
NORAD 40960
ARIRANG-1 (KOMPSAT-1)
NORAD 26032
0.335 14.91 1.4e-05
2026-10-12 21:32:14 LINGQIAO VIDEO B
NORAD 40960
ARIRANG-1 (KOMPSAT-1)
NORAD 26032
3.520 14.91 1.3e-07
2026-10-13 00:12:52 LINGQIAO VIDEO B
NORAD 40960
KUIPER-00617
NORAD 69776
3.455 14.18 1.7e-07
2026-10-13 08:22:56 LINGQIAO VIDEO B
NORAD 40960
KUIPER-00018
NORAD 63733
2.433 8.75 6.2e-07
2026-10-13 17:38:07 LINGQIAO VIDEO B
NORAD 40960
UNISAT-2
NORAD 27608
1.815 11.50 9.3e-07
2026-10-14 01:32:16 LINGQIAO VIDEO B
NORAD 40960
SL-12 DEB
NORAD 29325
4.727 12.25 1.4e-07
2026-10-14 12:11:18 LINGQIAO VIDEO B
NORAD 40960
CZ-6A DEB
NORAD 55214
4.319 7.80 2.1e-07
2026-10-14 18:32:24 LINGQIAO VIDEO B
NORAD 40960
KUIPER-00532
NORAD 69604
2.966 10.63 3.7e-07
2026-10-14 23:10:34 LINGQIAO VIDEO B
NORAD 40960
COSMOS 2251 DEB
NORAD 34129
1.898 15.04 4.2e-07
2026-10-15 12:34:43 LINGQIAO VIDEO B
NORAD 40960
KINEIS-1B
NORAD 60079
2.514 4.30 6.7e-07
2026-10-15 15:58:15 LINGQIAO VIDEO B
NORAD 40960
SL-24 DEB
NORAD 36602
3.112 14.47 1.9e-07
2026-10-15 19:02:16 LINGQIAO VIDEO B
NORAD 40960
CZ-4B DEB
NORAD 26329
3.864 12.45 1.9e-07
2026-10-16 20:40:25 LINGQIAO VIDEO B
NORAD 40960
KUIPER-00124
NORAD 65953
3.736 14.56 1.3e-07
2026-10-16 23:59:20 LINGQIAO VIDEO B
NORAD 40960
KUIPER-00617
NORAD 69776
1.170 14.54 1.3e-06
2026-10-17 02:51:41 LINGQIAO VIDEO B
NORAD 40960
FORMOSAT-3 FM3
NORAD 29050
3.893 13.58 1.5e-07
2026-10-17 14:45:13 LINGQIAO VIDEO B
NORAD 40960
KUIPER-00170
NORAD 65783
2.687 13.95 3.0e-07
2026-10-18 02:17:08 LINGQIAO VIDEO B
NORAD 40960
COSMOS 2251 DEB
NORAD 35476
3.481 12.52 2.3e-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