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 23088.32688349 .00000610 00000-0 54286-3 0 9990
2 00082 38.8623 40.8175 1167041 301.2418 47.9025 12.26149558932370
| Epoch (UTC): | 29 March 2023 07:50:42 |
| Eccentricity: | 0.1167041 |
| inclination: | 38.8623° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 40.8175° |
| argument of perigee: | 301.2418° |
| revolutions per day: | 12.26149558 |
| mean anomaly at epoch: | 47.9025° |
| orbit number at epoch: | 93237 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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