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 27133U 01049CD 24357.81305037 .00002388 00000-0 42163-3 0 9998
2 27133 97.6965 309.3733 0042767 166.4801 193.7562 14.67708941226853
| Epoch (UTC): | 22 December 2024 19:30:47 |
| Eccentricity: | 0.0042767 |
| inclination: | 97.6965° |
| perigee height: | 638 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 309.3733° |
| argument of perigee: | 166.4801° |
| revolutions per day: | 14.67708941 |
| mean anomaly at epoch: | 193.7562° |
| orbit number at epoch: | 22685 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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