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

HMU-SAT2

In orbit NORAD 67687 UNBL-8646-7261-0218-2058 Japan

0

Observations all time

Mission information
Spacecraft name
HMU-SAT2
Other names
Teruteru
Deployer
XSKZ-5603-1870-9019-3066
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
2025-10-26 00:00:00
Separation time
2026-02-03 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
304.35 km
Apogee
319.61 km
Inclination
51.6°
Period
90.8 min
Semi-major axis
6690.1 km
Velocity
7.72 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 22:09:14 UTC
Two-line elements (TLE)
1 67687U 98067YE  26286.61761830  .00445036  00000-0  16163-2 0  9991
2 67687 51.6208 49.8055 0011405 309.3308 50.6684 15.86729551 38803
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.