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 62391U 26145.61416263 +.00000000 +00000-0 +65791-3 0 00002
2 62391 44.9758 28.9158 0006800 205.6385 154.4168 15.44767006 05
| Epoch (UTC): | 25 May 2026 14:44:23 |
| Eccentricity: | 0.0006800 |
| inclination: | 44.9758° |
| perigee height: | 427 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 28.9158° |
| argument of perigee: | 205.6385° |
| revolutions per day: | 15.44767006 |
| mean anomaly at epoch: | 154.4168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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