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 23270.04411652 .00000654 00000-0 22154-3 0 9990
2 20978 98.7484 301.3323 0072686 5.3112 354.8830 14.38738867719737
| Epoch (UTC): | 27 September 2023 01:03:31 |
| Eccentricity: | 0.0072686 |
| inclination: | 98.7484° |
| perigee height: | 711 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 301.3323° |
| argument of perigee: | 5.3112° |
| revolutions per day: | 14.38738867 |
| mean anomaly at epoch: | 354.8830° |
| orbit number at epoch: | 71973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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