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 30599U 99025AME 24357.51627256 .00004638 00000-0 14425-2 0 9995
2 30599 98.6189 12.7192 0309030 290.8006 66.0323 14.17492318921306
| Epoch (UTC): | 22 December 2024 12:23:25 |
| Eccentricity: | 0.0309030 |
| inclination: | 98.6189° |
| perigee height: | 611 km |
| apogee height: | 1057 km |
| right ascension of ascending node: | 12.7192° |
| argument of perigee: | 290.8006° |
| revolutions per day: | 14.17492318 |
| mean anomaly at epoch: | 66.0323° |
| orbit number at epoch: | 92130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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