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TriSat-4

Re-entered NORAD 67482 KUVZ-8479-4916-9498-7090 ОКБ5 Russia

Satellite appearance

Soyuz 2.1b Fregat-M

Carrier rocket

Cosmodrome Site 1S

Spaceport

0

Observations all time

Mission information
Spacecraft name
TriSat-4
Deployer
WVCI-2338-9266-5261-4671
Status
Inactive
The satellite burned up in the atmosphere
Launch and timeline
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2025-12-28 13:18:05
Separation time
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
264.64 km
Apogee
278.98 km
Inclination
97.4°
Period
90.0 min
Semi-major axis
6649.9 km
Velocity
1.32 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-08-19 20:35:45 UTC
Two-line elements (TLE)
1 67482U 25313BE  26231.17427717  .01297284  89973-3  26073-2 0  9993
2 67482 97.3670 311.8103 0010785 264.2748 95.7300 15.99807030 33138
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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.