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 00116U 61015A 21055.41638016 -.00000029 00000-0 37090-4 0 9998
2 00116 66.8108 312.2515 0077157 197.2441 162.6016 13.91784195 26887
| Epoch (UTC): | 24 February 2021 09:59:35 |
| Eccentricity: | 0.0077157 |
| inclination: | 66.8108° |
| perigee height: | 866 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 312.2515° |
| argument of perigee: | 197.2441° |
| revolutions per day: | 13.91784195 |
| mean anomaly at epoch: | 162.6016° |
| orbit number at epoch: | 2688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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