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GAOFEN 2

In orbit NORAD 40118 NEOU-7691-1418-9175-1889 China

2014

Launch

0

Observations all time

Mission information
Spacecraft name
GAOFEN 2
Other names
2014-049A
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
2014-08-19 00:00:00
Separation time
2014-08-19 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
618.62 km
Apogee
627.66 km
Inclination
98.0°
Period
97.2 min
Semi-major axis
7001.3 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:36 UTC
Two-line elements (TLE)
1 40118U 14049A   26283.98225975 -.00000002  00000-0  66804-5 0  9992
2 40118 97.9996 348.0065 0006454 208.8715 151.2141 14.81022670656374
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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 17:38:46 GAOFEN-2
NORAD 40118
KUIPER-00606
NORAD 69289
3.658 12.32 2.1e-07
2026-10-11 19:07:49 GAOFEN-2
NORAD 40118
KUIPER-00214
NORAD 67778
3.772 6.40 2.8e-07
2026-10-12 07:33:33 GAOFEN-2
NORAD 40118
NOAA 16 DEB
NORAD 41419
4.645 10.36 1.6e-07
2026-10-13 03:50:59 GAOFEN-2
NORAD 40118
CZ-4B R/B
NORAD 40337
0.824 5.44 6.1e-06
2026-10-13 11:53:29 IRIS
NORAD 39197
GAOFEN-2
NORAD 40118
2.545 13.79 3.5e-07
2026-10-13 16:14:18 GAOFEN-2
NORAD 40118
KUIPER-00526
NORAD 69764
3.327 13.86 2.0e-07
2026-10-14 00:04:36 GAOFEN-2
NORAD 40118
CSG-3
NORAD 67304
1.915 12.78 7.2e-07
2026-10-14 01:50:00 YAOGAN-4
NORAD 33446
GAOFEN-2
NORAD 40118
4.055 13.59 1.4e-07
2026-10-14 08:15:18 GAOFEN-2
NORAD 40118
DMSP 5D-3 F16 DEB
NORAD 28081
4.433 2.58 2.2e-07
2026-10-14 11:39:39 GAOFEN-2
NORAD 40118
FENGYUN 1C DEB
NORAD 38789
2.860 14.71 2.1e-07
2026-10-14 12:06:22 GAOFEN-2
NORAD 40118
KUIPER-00116
NORAD 65153
4.505 9.36 1.8e-07
2026-10-14 13:43:40 GAOFEN-2
NORAD 40118
KUIPER-00116
NORAD 65153
3.103 9.38 3.7e-07
2026-10-14 15:20:59 GAOFEN-2
NORAD 40118
KUIPER-00116
NORAD 65153
4.872 9.41 1.5e-07
2026-10-15 01:09:08 GAOFEN-2
NORAD 40118
COSMOS 2251 DEB
NORAD 36369
3.008 14.87 1.8e-07
2026-10-15 23:28:13 GAOFEN-2
NORAD 40118
COSMOS 2251 DEB
NORAD 36045
2.499 15.04 2.4e-07
2026-10-16 07:18:57 GAOFEN-2
NORAD 40118
GAOFEN-10R
NORAD 44622
2.776 12.17 3.7e-07
2026-10-16 07:19:13 GAOFEN-2
NORAD 40118
NOAA 16 DEB
NORAD 41372
4.845 12.19 1.2e-07
2026-10-16 07:49:00 GAOFEN-2
NORAD 40118
KUIPER-00533
NORAD 69605
3.559 14.30 1.6e-07
2026-10-16 07:54:05 GAOFEN-2
NORAD 40118
KUIPER-00452
NORAD 68946
2.838 12.88 3.3e-07
2026-10-16 17:33:42 GAOFEN-2
NORAD 40118
KUIPER-00019
NORAD 63734
3.969 14.21 1.3e-07
2026-10-16 23:30:37 HUANJING 1A (HJ-1A)
NORAD 33320
GAOFEN-2
NORAD 40118
4.183 9.86 2.0e-07
2026-10-17 04:58:07 GAOFEN-2
NORAD 40118
KUIPER-00416
NORAD 68931
2.732 13.41 3.2e-07
2026-10-17 09:26:28 GAOFEN-2
NORAD 40118
KUIPER-00151
NORAD 65771
3.769 14.09 1.5e-07
2026-10-17 13:03:41 GAOFEN-2
NORAD 40118
KUIPER-00527
NORAD 69269
3.004 13.74 2.5e-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