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 19976U 89035A 22235.84347697 0.00000000 00000-0 00000-0 0 02
2 19976 7.7980 6.4532 0944087 317.3107 35.7262 1.00270000 04
| Epoch (UTC): | 23 August 2022 20:14:36 |
| Eccentricity: | 0.0944087 |
| inclination: | 7.7980° |
| perigee height: | 31806 km |
| apogee height: | 39767 km |
| right ascension of ascending node: | 6.4532° |
| argument of perigee: | 317.3107° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 35.7262° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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