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 60902U 24140LH 24357.90503312 .00005521 00000-0 12214-2 0 9997
2 60902 89.0458 335.4914 0118886 325.1905 34.1566 14.52788453 18369
| Epoch (UTC): | 22 December 2024 21:43:14 |
| Eccentricity: | 0.0118886 |
| inclination: | 89.0458° |
| perigee height: | 632 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 335.4914° |
| argument of perigee: | 325.1905° |
| revolutions per day: | 14.52788453 |
| mean anomaly at epoch: | 34.1566° |
| orbit number at epoch: | 1836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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