RU | EN | ZH --:-- UTC Sign in

CBERS-4A

In orbit NORAD 44879 ETAK-6320-1090-8842-1318 Brazil China

2019

Launch

0

Observations all time

Mission information
Spacecraft name
CBERS-4A
Other names
2019-093A
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
2019-12-20 00:00:00
Separation time
2019-12-20 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
568.55 km
Apogee
584.73 km
Inclination
97.8°
Period
96.3 min
Semi-major axis
6954.8 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:56 UTC
Two-line elements (TLE)
1 44879U 19093A   26283.56034547  .00002569  00000-0  23461-3 0  9990
2 44879 97.7754 6.5623 0011582 33.8430 326.3528 14.95889771369290
Copy content
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 02:32:51 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-6043
NORAD 56464
1.977 6.76 3.1e-05
2026-10-11 02:46:56 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-3055
NORAD 49137
2.409 10.58 1.7e-05
2026-10-12 03:13:46 TIANQIN 1 (CAS-6)
NORAD 44879
KUIPER-00557
NORAD 69622
3.673 14.56 1.4e-07
2026-10-12 22:26:09 TIANQIN 1 (CAS-6)
NORAD 44879
COSMOS 2251 DEB
NORAD 38208
2.431 15.09 2.5e-07
2026-10-13 02:24:05 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-35882
NORAD 67088
4.855 15.06 2.0e-06
2026-10-13 11:23:57 TIANQIN 1 (CAS-6)
NORAD 44879
FOREST-16 (SOWITASGOHT)
NORAD 68998
1.443 14.95 7.7e-07
2026-10-13 15:41:25 TIANQIN 1 (CAS-6)
NORAD 44879
PEGASUS DEB
NORAD 39917
3.284 15.20 1.4e-07
2026-10-13 21:58:30 TIANQIN 1 (CAS-6)
NORAD 44879
GRUS-1C
NORAD 47933
4.140 14.69 1.0e-07
2026-10-14 02:13:33 TIANQIN 1 (CAS-6)
NORAD 44879
ESSAIM-3
NORAD 28496
4.623 14.06 9.9e-08
2026-10-14 02:56:19 TIANQIN 1 (CAS-6)
NORAD 44879
SKYKRAFT-4D
NORAD 64898
4.205 2.76 2.5e-07
2026-10-14 04:37:57 TIANQIN 1 (CAS-6)
NORAD 44879
ESSAIM-3
NORAD 28496
3.225 14.09 2.0e-07
2026-10-14 08:49:40 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-36200
NORAD 67101
4.213 15.03 2.7e-06
2026-10-14 10:25:47 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-36166
NORAD 67084
4.354 15.02 2.5e-06
2026-10-14 13:48:35 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-5321
NORAD 55302
2.701 15.07 6.4e-06
2026-10-14 17:09:09 TIANQIN 1 (CAS-6)
NORAD 44879
LEMUR-2-DELOITTE-1
NORAD 63259
2.830 14.94 2.0e-07
2026-10-14 21:46:39 FORMOSAT 7-5
NORAD 44358
TIANQIN 1 (CAS-6)
NORAD 44879
4.894 13.21 1.0e-07
2026-10-15 06:21:56 TIANQIN 1 (CAS-6)
NORAD 44879
SNUGLITE-III
NORAD 66661
4.951 14.65 7.4e-08
2026-10-15 14:01:33 TIANQIN 1 (CAS-6)
NORAD 44879
LEMUR-2-LIA-MARTIN
NORAD 63248
3.096 14.93 1.7e-07
2026-10-16 03:00:43 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-5634
NORAD 55439
2.040 12.03 2.1e-05
2026-10-16 19:03:02 TIANQIN 1 (CAS-6)
NORAD 44879
STARLINK-34667
NORAD 64815
4.920 9.68 4.4e-06
2026-10-16 21:37:56 TIANQIN 1 (CAS-6)
NORAD 44879
METEOR 2-1 DEB
NORAD 38532
4.463 6.99 2.0e-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