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 62957U 26145.53648759 +.00000000 +00000-0 +24132-3 0 00002
2 62957 53.1590 235.4812 0000883 66.1609 293.9485 15.31706056 00
| Epoch (UTC): | 25 May 2026 12:52:32 |
| Eccentricity: | 0.0000883 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.4812° |
| argument of perigee: | 66.1609° |
| revolutions per day: | 15.31706056 |
| mean anomaly at epoch: | 293.9485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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