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 35937U 09052A 23271.11385604 0.00000050 00000-0 20884-3 0 09
2 35937 57.9876 286.6338 0008669 190.9836 169.0164 12.83511168 05
| Epoch (UTC): | 28 September 2023 02:43:57 |
| Eccentricity: | 0.0008669 |
| inclination: | 57.9876° |
| perigee height: | 1321 km |
| apogee height: | 1334 km |
| right ascension of ascending node: | 286.6338° |
| argument of perigee: | 190.9836° |
| revolutions per day: | 12.83511168 |
| mean anomaly at epoch: | 169.0164° |
| 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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