View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 21799U 91076C 25131.43129596 .00006353 00000-0 53867-3 0 9991
2 21799 63.2966 140.4703 0892299 65.4986 303.6411 13.55786189 49013
Epoch (UTC): | 11 May 2025 10:21:03 |
Eccentricity: | 0.0892299 |
inclination: | 63.2966° |
perigee height: | 388 km |
apogee height: | 1714 km |
right ascension of ascending node: | 140.4703° |
argument of perigee: | 65.4986° |
revolutions per day: | 13.55786189 |
mean anomaly at epoch: | 303.6411° |
orbit number at epoch: | 4901 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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