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 00045U 60007A 21016.84195090 -.00000062 00000-0 11502-4 0 9990
2 00045 66.6933 178.5335 0253244 161.8966 199.1361 14.33702075 96426
Epoch (UTC): | 16 January 2021 20:12:24 |
Eccentricity: | 0.0253244 |
inclination: | 66.6933° |
perigee height: | 598 km |
apogee height: | 960 km |
right ascension of ascending node: | 178.5335° |
argument of perigee: | 161.8966° |
revolutions per day: | 14.33702075 |
mean anomaly at epoch: | 199.1361° |
orbit number at epoch: | 9642 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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