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 04216U 69082CF 24357.83163327 .00000942 00000-0 42858-3 0 9997
2 04216 70.1050 167.3490 0046900 164.8530 195.4008 14.24078328 84260
| Epoch (UTC): | 22 December 2024 19:57:33 |
| Eccentricity: | 0.0046900 |
| inclination: | 70.1050° |
| perigee height: | 778 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 167.3490° |
| argument of perigee: | 164.8530° |
| revolutions per day: | 14.24078328 |
| mean anomaly at epoch: | 195.4008° |
| orbit number at epoch: | 8426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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