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 42791U 17036AC 24004.55647480 .15932835 20937-5 23518-3 0 9993
2 42791 97.0833 50.4615 0004059 337.7263 22.3865 16.48851198364522
| Epoch (UTC): | 04 January 2024 13:21:19 |
| Eccentricity: | 0.0004059 |
| inclination: | 97.0833° |
| perigee height: | 140 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 50.4615° |
| argument of perigee: | 337.7263° |
| revolutions per day: | 16.48851198 |
| mean anomaly at epoch: | 22.3865° |
| orbit number at epoch: | 36452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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