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HJ 2F

In orbit NORAD 57519 OCRC-3744-9518-2127-6987 China

2023

Launch

1

Observations all time

Mission information
Spacecraft name
HJ 2F
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
2023-08-08 00:00:00
Separation time
2023-08-08 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
495.60 km
Apogee
508.40 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6880.1 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:56 UTC
Two-line elements (TLE)
1 57519U 23116A   26283.64334995  .00006196  00000-0  28820-3 0  9999
2 57519 97.3887 286.8012 0009316 117.8916 242.3264 15.20270215176316
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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 16:46:55 HJ-2F
NORAD 57519
OBJECT AG
NORAD 67278
2.144 8.61 8.1e-07
2026-10-13 00:40:42 HJ-2F
NORAD 57519
JAY-D2
NORAD 62665
0.906 9.03 4.5e-06
2026-10-13 03:49:43 JILIN-1 09
NORAD 43943
HJ-2F
NORAD 57519
3.457 10.77 2.8e-07
2026-10-14 01:21:20 STARLINK-5926
NORAD 55944
HJ-2F
NORAD 57519
4.806 14.93 2.2e-06
2026-10-14 07:35:21 STARLINK-5072
NORAD 55758
HJ-2F
NORAD 57519
4.791 13.29 3.3e-06
2026-10-14 08:16:24 HJ-2F
NORAD 57519
ACCENTURE-1
NORAD 66767
3.695 8.50 2.8e-07
2026-10-15 03:10:34 HJ-2F
NORAD 57519
VSP RF A1
NORAD 59135
1.588 13.91 8.9e-07
2026-10-15 03:13:43 HJ-2F
NORAD 57519
ANISCSAT-1
NORAD 66671
2.076 8.57 8.7e-07
2026-10-15 04:01:08 HJ-2F
NORAD 57519
OBJECT Q
NORAD 61908
1.823 8.30 1.1e-06
2026-10-16 03:52:01 STARLINK-5917
NORAD 55942
HJ-2F
NORAD 57519
3.562 14.76 4.2e-06
2026-10-16 05:14:52 HJ-2F
NORAD 57519
FENGYUN 1C DEB
NORAD 31877
4.764 13.22 1.1e-07
2026-10-16 08:26:31 HJ-2F
NORAD 57519
OKEAN-2
NORAD 20510
4.792 15.18 8.4e-07
2026-10-16 10:01:24 HJ-2F
NORAD 57519
OKEAN-2
NORAD 20510
2.016 15.18 4.7e-06
2026-10-16 11:36:16 HJ-2F
NORAD 57519
OKEAN-2
NORAD 20510
0.763 15.18 3.3e-05
2026-10-16 13:11:09 HJ-2F
NORAD 57519
OKEAN-2
NORAD 20510
3.067 15.18 2.0e-06
2026-10-16 13:16:52 STARLINK-4624
NORAD 53684
HJ-2F
NORAD 57519
4.231 13.67 3.9e-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