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 39249U 13048A 23088.45018332 .00000055 00000-0 32577-3 0 9997
2 39249 82.4886 356.3106 0015307 259.0606 100.8750 12.42872360432985
Epoch (UTC): | 29 March 2023 10:48:15 |
Eccentricity: | 0.0015307 |
inclination: | 82.4886° |
perigee height: | 1482 km |
apogee height: | 1506 km |
right ascension of ascending node: | 356.3106° |
argument of perigee: | 259.0606° |
revolutions per day: | 12.42872360 |
mean anomaly at epoch: | 100.8750° |
orbit number at epoch: | 43298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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