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 05042U 71015P 23341.37739539 .00006582 00000-0 18160-2 0 9993
2 05042 65.6152 350.6409 0626992 2.7745 357.6531 13.70186047524765
| Epoch (UTC): | 07 December 2023 09:03:26 |
| Eccentricity: | 0.0626992 |
| inclination: | 65.6152° |
| perigee height: | 536 km |
| apogee height: | 1461 km |
| right ascension of ascending node: | 350.6409° |
| argument of perigee: | 2.7745° |
| revolutions per day: | 13.70186047 |
| mean anomaly at epoch: | 357.6531° |
| orbit number at epoch: | 52476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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