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 05301U 71035D 24357.68992517 .00008624 00000-0 11306-2 0 9996
2 05301 74.0264 222.0538 0010516 180.8950 179.2209 14.80418125831545
| Epoch (UTC): | 22 December 2024 16:33:29 |
| Eccentricity: | 0.0010516 |
| inclination: | 74.0264° |
| perigee height: | 620 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 222.0538° |
| argument of perigee: | 180.8950° |
| revolutions per day: | 14.80418125 |
| mean anomaly at epoch: | 179.2209° |
| orbit number at epoch: | 83154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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