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 35789U 93036ASK 24357.60747652 .00000502 00000-0 18071-3 0 9998
2 35789 74.0370 216.0445 0047367 42.8409 317.6418 14.35599723561304
| Epoch (UTC): | 22 December 2024 14:34:45 |
| Eccentricity: | 0.0047367 |
| inclination: | 74.0370° |
| perigee height: | 739 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 216.0445° |
| argument of perigee: | 42.8409° |
| revolutions per day: | 14.35599723 |
| mean anomaly at epoch: | 317.6418° |
| orbit number at epoch: | 56130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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