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 62959U 26145.63577815 +.00000000 +00000-0 +94374-3 0 00004
2 62959 53.1593 235.3869 0000598 88.5078 271.5991 15.30207031 09
| Epoch (UTC): | 25 May 2026 15:15:31 |
| Eccentricity: | 0.0000598 |
| inclination: | 53.1593° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3869° |
| argument of perigee: | 88.5078° |
| revolutions per day: | 15.30207031 |
| mean anomaly at epoch: | 271.5991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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