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 07210U 74011B 24283.77938266 .00000299 00000-0 14811-3 0 9998
2 07210 81.2344 311.3095 0080068 340.3170 19.4916 14.13437667607045
| Epoch (UTC): | 09 October 2024 18:42:18 |
| Eccentricity: | 0.0080068 |
| inclination: | 81.2344° |
| perigee height: | 790 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 311.3095° |
| argument of perigee: | 340.3170° |
| revolutions per day: | 14.13437667 |
| mean anomaly at epoch: | 19.4916° |
| orbit number at epoch: | 60704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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