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 36416U 10009D 21104.60046540 -.00000085 00000-0 12206-4 0 9992
2 36416 63.4188 111.1072 0524686 355.5349 4.1100 13.69590638555584
| Epoch (UTC): | 14 April 2021 14:24:40 |
| Eccentricity: | 0.0524686 |
| inclination: | 63.4188° |
| perigee height: | 614 km |
| apogee height: | 1388 km |
| right ascension of ascending node: | 111.1072° |
| argument of perigee: | 355.5349° |
| revolutions per day: | 13.69590638 |
| mean anomaly at epoch: | 4.1100° |
| orbit number at epoch: | 55558 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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