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 27880U 66025H 24284.99023980 .00406971 00000-0 51668-1 0 9998
2 27880 144.5962 329.8562 0005803 236.8639 123.1512 14.78558432134714
| Epoch (UTC): | 10 October 2024 23:45:56 |
| Eccentricity: | 0.0005803 |
| inclination: | 144.5962° |
| perigee height: | 630 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 329.8562° |
| argument of perigee: | 236.8639° |
| revolutions per day: | 14.78558432 |
| mean anomaly at epoch: | 123.1512° |
| orbit number at epoch: | 13471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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