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 23087.34914785 .00000539 00000-0 48236-3 0 9995
2 00082 38.8625 44.4364 1167101 296.5277 52.0414 12.26148126932254
| Epoch (UTC): | 28 March 2023 08:22:46 |
| Eccentricity: | 0.1167101 |
| inclination: | 38.8625° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 44.4364° |
| argument of perigee: | 296.5277° |
| revolutions per day: | 12.26148126 |
| mean anomaly at epoch: | 52.0414° |
| orbit number at epoch: | 93225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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