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 00082U 61004B 23091.26016671 .00000585 00000-0 52579-3 0 9994
2 00082 38.8612 29.9601 1166815 315.3881 35.8449 12.26152711932739
| Epoch (UTC): | 01 April 2023 06:14:38 |
| Eccentricity: | 0.1166815 |
| inclination: | 38.8612° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 29.9601° |
| argument of perigee: | 315.3881° |
| revolutions per day: | 12.26152711 |
| mean anomaly at epoch: | 35.8449° |
| orbit number at epoch: | 93273 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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