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 20978U 90105A 23081.07724740 .00000482 00000-0 16794-3 0 9990
2 20978 98.7648 108.5561 0072524 204.0614 155.7179 14.38533377692560
| Epoch (UTC): | 22 March 2023 01:51:14 |
| Eccentricity: | 0.0072524 |
| inclination: | 98.7648° |
| perigee height: | 711 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 108.5561° |
| argument of perigee: | 204.0614° |
| revolutions per day: | 14.38533377 |
| mean anomaly at epoch: | 155.7179° |
| orbit number at epoch: | 69256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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