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 23704U 95058A 24282.52803345 .00000517 00000-0 29894-3 0 9999
2 23704 70.9874 206.1595 0009689 357.0584 3.0479 14.13671070492968
| Epoch (UTC): | 08 October 2024 12:40:22 |
| Eccentricity: | 0.0009689 |
| inclination: | 70.9874° |
| perigee height: | 840 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 206.1595° |
| argument of perigee: | 357.0584° |
| revolutions per day: | 14.13671070 |
| mean anomaly at epoch: | 3.0479° |
| orbit number at epoch: | 49296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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