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 37855U 11061F 22221.68141749 .00008413 00000-0 36513-3 0 9993
2 37855 101.7152 8.9756 0151498 262.7346 95.6628 15.13037835589284
| Epoch (UTC): | 09 August 2022 16:21:14 |
| Eccentricity: | 0.0151498 |
| inclination: | 101.7152° |
| perigee height: | 422 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 8.9756° |
| argument of perigee: | 262.7346° |
| revolutions per day: | 15.13037835 |
| mean anomaly at epoch: | 95.6628° |
| orbit number at epoch: | 58928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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