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 38758U 12048A 21059.15959387 0.00000000 00000-0 00000-0 0 03
2 38758 63.4438 100.4263 0146870 359.4887 0.5113 13.40795848 06
Epoch (UTC): | 28 February 2021 03:49:48 |
Eccentricity: | 0.0146870 |
inclination: | 63.4438° |
perigee height: | 996 km |
apogee height: | 1216 km |
right ascension of ascending node: | 100.4263° |
argument of perigee: | 359.4887° |
revolutions per day: | 13.40795848 |
mean anomaly at epoch: | 0.5113° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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