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2025-012B

In orbit NORAD 62726 EYWK-8780-8758-9764-0550 China

2025

Launch

0

Observations all time

Mission information
Spacecraft name
2025-012B
Other names
2025-012B
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
2025-01-17 00:00:00
Separation time
2025-01-17 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
491.19 km
Apogee
501.84 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6874.7 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:39 UTC
Two-line elements (TLE)
1 62726U 25012B   26283.93633656  .00006159  00000-0  27189-3 0  9996
2 62726 97.4132 355.3724 0007742 222.7163 137.3472 15.22085089 95857
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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 06:25:59 OBJECT B
NORAD 62726
FLOCK 4H-7
NORAD 66710
2.692 0.03 6.1e-07
2026-10-13 17:32:04 OBJECT B
NORAD 62726
TRANSPORTER-13 OBJECT U
NORAD 63228
3.574 15.11 1.2e-07
2026-10-15 02:04:31 OBJECT B
NORAD 62726
HULIANWANG JISHU SHIYAN 9D
NORAD 68834
2.098 14.09 4.9e-07
2026-10-15 21:10:35 OBJECT B
NORAD 62726
OBJECT F
NORAD 63296
2.075 8.63 8.7e-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