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 30827U 99025AVM 24278.85689945 .00044502 00000-0 18260-1 0 9995
2 30827 98.9896 241.8294 0055683 8.0711 352.1350 14.25975182903358
| Epoch (UTC): | 04 October 2024 20:33:56 |
| Eccentricity: | 0.0055683 |
| inclination: | 98.9896° |
| perigee height: | 765 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 241.8294° |
| argument of perigee: | 8.0711° |
| revolutions per day: | 14.25975182 |
| mean anomaly at epoch: | 352.1350° |
| orbit number at epoch: | 90335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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