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 4368U 70027B 25162.90992538 -.00000395 00000-0 00000+0 0 9995
2 4368 86.1941 359.2669 7824343 72.0060 0.7294 0.21504509 36870
| Epoch (UTC): | 11 June 2025 21:50:17 |
| Eccentricity: | 0.7824343 |
| inclination: | 86.1941° |
| perigee height: | 19225 km |
| apogee height: | 203382 km |
| right ascension of ascending node: | 359.2669° |
| argument of perigee: | 72.0060° |
| revolutions per day: | 0.21504509 |
| mean anomaly at epoch: | 0.7294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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