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

HJ-2E

In orbit NORAD 54035 CWEB-1035-7024-6061-8210 China

2022

Launch

0

Observations all time

Mission information
Spacecraft name
HJ-2E
Other names
2022-132A
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
2022-10-12 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
498.57 km
Apogee
505.32 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6880.1 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:37 UTC
Two-line elements (TLE)
1 54035U 22132A   26283.93925876  .00010020  00000-0  46409-3 0  9996
2 54035 97.3845 286.1819 0004908 353.7324 6.3849 15.20284654222023
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
2026-10-12 00:55:31 HJ-2E
NORAD 54035
BLACKJACK ACES-2
NORAD 56955
3.957 13.87 1.4e-07
2026-10-12 06:28:02 HJ-2E
NORAD 54035
OBJECT C
NORAD 67748
3.023 13.41 2.7e-07
2026-10-13 02:29:33 HJ-2E
NORAD 54035
RAWHIDE-1
NORAD 68629
1.963 14.64 4.8e-07
2026-10-13 03:02:15 COSMOS 2538
NORAD 44424
HJ-2E
NORAD 54035
4.872 9.50 1.5e-07
2026-10-13 18:39:39 HJ-2E
NORAD 54035
SPACEMOBILE-006
NORAD 67232
4.909 14.01 9.1e-08
2026-10-14 08:50:44 SINOD-D 3
NORAD 40977
HJ-2E
NORAD 54035
0.633 5.39 1.0e-05
2026-10-14 16:11:12 HJ-2E
NORAD 54035
UNKNOWN
NORAD 270100
4.918 1.16 1.8e-07
2026-10-14 16:57:04 HJ-2E
NORAD 54035
GARAI-A
NORAD 62635
4.670 9.18 1.7e-07
2026-10-14 17:44:37 HJ-2E
NORAD 54035
TRANSPORTER-15 OBJECT L
NORAD 66676
0.823 8.53 5.5e-06
2026-10-14 18:31:59 HJ-2E
NORAD 54035
TRANSPORTER-15 OBJECT L
NORAD 66676
4.520 8.54 1.8e-07
2026-10-15 01:46:12 HJ-2E
NORAD 54035
PREFIRE-2
NORAD 59881
1.184 14.49 1.4e-06
2026-10-15 07:12:22 HJ-2E
NORAD 54035
NUSAT-53 (JANE GOODALL)
NORAD 68432
1.724 5.79 1.4e-06
2026-10-15 15:51:08 HJ-2E
NORAD 54035
MACSAT (FINCH 1)
NORAD 58024
1.308 9.73 2.1e-06
2026-10-15 21:20:42 HJ-2E
NORAD 54035
COSMOS 2251 DEB
NORAD 34856
3.451 13.60 2.0e-07
2026-10-15 22:10:35 HJ-2E
NORAD 54035
PIAST-M
NORAD 66758
2.546 8.60 5.8e-07
2026-10-15 22:57:56 HJ-2E
NORAD 54035
PIAST-M
NORAD 66758
4.460 8.61 1.9e-07
2026-10-16 02:07:21 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
4.455 9.16 1.8e-07
2026-10-16 03:42:07 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
2.286 9.16 7.0e-07
2026-10-16 04:29:40 HJ-2E
NORAD 54035
LEO EXPRESS 3
NORAD 66687
3.953 8.64 2.4e-07
2026-10-16 05:16:54 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
1.893 9.16 1.0e-06
2026-10-16 06:04:18 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
3.461 9.14 3.0e-07
2026-10-16 06:51:41 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
3.885 9.16 2.4e-07
2026-10-16 07:39:05 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
2.345 9.14 6.6e-07
2026-10-16 09:13:52 HJ-2E
NORAD 54035
CO3D 1
NORAD 64903
3.538 9.14 2.9e-07
2026-10-16 10:03:33 HJ-2E
NORAD 54035
VIREON-1
NORAD 68434
1.570 5.78 1.7e-06

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