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 36105U 09066B 21014.19556023 0.00000800 00000-0 41973-4 0 04
2 36105 97.2869 12.3996 0030197 115.5250 244.4748 15.15389542 03
Epoch (UTC): | 14 January 2021 04:41:36 |
Eccentricity: | 0.0030197 |
inclination: | 97.2869° |
perigee height: | 499 km |
apogee height: | 540 km |
right ascension of ascending node: | 12.3996° |
argument of perigee: | 115.5250° |
revolutions per day: | 15.15389542 |
mean anomaly at epoch: | 244.4748° |
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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