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Luojia-1

In orbit NORAD 43485 QWJS-4478-4513-2046-4348 China

2018

Launch

35

Observations all time

Mission information
Spacecraft name
Luojia-1
Other names
LUOJIA 1-01, LUOJIA 1A
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
2018-06-02 00:00:00
Separation time
Last observers
Observer
Time of receipt
2024-03-19 20:24:07 UTC
2024-03-13 20:00:20 UTC
2024-02-16 10:01:23 UTC
2024-02-10 22:20:02 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
595.24 km
Apogee
609.62 km
Inclination
97.8°
Period
96.8 min
Semi-major axis
6980.6 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 43485U 18048B   26283.60952274  .00000920  00000-0  10710-3 0  9994
2 43485 97.8029 359.9141 0010290 100.0535 260.1843 14.87612628451378
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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 12:03:21 LUOJIA-1 01
NORAD 43485
ONEWEB-0050
NORAD 45453
2.050 14.34 1.5e-06
2026-10-11 22:03:49 LUOJIA-1 01
NORAD 43485
FIRESAT3
NORAD 69890
3.206 14.97 1.5e-07
2026-10-11 23:40:37 LUOJIA-1 01
NORAD 43485
FIRESAT3
NORAD 69890
2.897 14.97 1.9e-07
2026-10-12 03:22:56 LUOJIA-1 01
NORAD 43485
AETHER-7
NORAD 67378
3.322 9.59 3.2e-07
2026-10-12 04:51:19 SINOD-D 3
NORAD 40977
LUOJIA-1 01
NORAD 43485
2.330 11.05 5.9e-07
2026-10-12 21:08:07 LUOJIA-1 01
NORAD 43485
FENGYUN 1C DEB
NORAD 31175
3.136 7.84 3.9e-07
2026-10-12 21:55:40 LUOJIA-1 01
NORAD 43485
PSLV DEB
NORAD 27130
3.799 2.28 3.0e-07
2026-10-14 21:36:14 LUOJIA-1 01
NORAD 43485
H-2A R/B
NORAD 64695
4.423 13.07 1.3e-07
2026-10-15 01:23:58 LUOJIA-1 01
NORAD 43485
COSMOS 2251 DEB
NORAD 33799
3.858 15.03 1.0e-07
2026-10-15 13:41:17 LUOJIA-1 01
NORAD 43485
FALCON EYE 2
NORAD 47226
2.274 0.42 8.5e-07
2026-10-15 23:49:37 LUOJIA-1 01
NORAD 43485
DELTA 1 DEB
NORAD 10626
4.383 13.58 1.3e-07
2026-10-16 04:21:46 LUOJIA-1 01
NORAD 43485
COSMOS 2251 DEB
NORAD 35793
2.777 14.95 2.0e-07
2026-10-16 07:51:27 LUOJIA-1 01
NORAD 43485
GEESAT-1 01
NORAD 52785
4.277 6.13 2.2e-07
2026-10-16 11:01:52 LUOJIA-1 01
NORAD 43485
FIRESAT3
NORAD 69890
3.970 14.97 1.0e-07
2026-10-16 12:38:47 LUOJIA-1 01
NORAD 43485
FIRESAT3
NORAD 69890
2.456 14.97 2.6e-07
2026-10-16 13:23:17 LUOJIA-1 01
NORAD 43485
IRIDIUM 33 DEB
NORAD 35797
4.813 15.11 6.4e-08

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