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 is defined by the following mean orbital elements,
1 04366U 70027A 25162.89116127 -.00000305 00000-0 00000-0 0 9995
2 04366 87.5969 0.9935 7753526 72.3352 1.1488 0.21456810 40573
| Epoch (UTC): | 11 June 2025 21:23:16 |
| Eccentricity: | 0.7753526 |
| inclination: | 87.5969° |
| perigee height: | 20098 km |
| apogee height: | 202859 km |
| right ascension of ascending node: | 0.9935° |
| argument of perigee: | 72.3352° |
| revolutions per day: | 0.21456810 |
| mean anomaly at epoch: | 1.1488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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