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 36714U 99025EAL 22221.39616359 .00001228 00000-0 62178-3 0 9997
2 36714 98.7704 286.9910 0032895 354.5602 5.5211 14.17657631717375
| Epoch (UTC): | 09 August 2022 09:30:28 |
| Eccentricity: | 0.0032895 |
| inclination: | 98.7704° |
| perigee height: | 809 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 286.9910° |
| argument of perigee: | 354.5602° |
| revolutions per day: | 14.17657631 |
| mean anomaly at epoch: | 5.5211° |
| orbit number at epoch: | 71737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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