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 38528U 12034A 22277.00136979 0.00000000 00000-0 00000-0 0 04
2 38528 4.1357 68.8750 0017991 357.8129 2.1871 1.00270000 03
| Epoch (UTC): | 04 October 2022 00:01:58 |
| Eccentricity: | 0.0017991 |
| inclination: | 4.1357° |
| perigee height: | 35711 km |
| apogee height: | 35862 km |
| right ascension of ascending node: | 68.8750° |
| argument of perigee: | 357.8129° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 2.1871° |
| 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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