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 00721U 63053B 24357.86361472 .00000803 00000-0 47026-3 0 9998
2 00721 78.6034 284.7623 1088027 54.5920 315.1938 12.54651735782155
| Epoch (UTC): | 22 December 2024 20:43:36 |
| Eccentricity: | 0.1088027 |
| inclination: | 78.6034° |
| perigee height: | 594 km |
| apogee height: | 2296 km |
| right ascension of ascending node: | 284.7623° |
| argument of perigee: | 54.5920° |
| revolutions per day: | 12.54651735 |
| mean anomaly at epoch: | 315.1938° |
| orbit number at epoch: | 78215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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