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 62695U 26145.45450615 +.00000000 +00000-0 +70580-4 0 00003
2 62695 97.7079 223.7604 0004263 83.4394 276.7311 14.93150613 09
| Epoch (UTC): | 25 May 2026 10:54:29 |
| Eccentricity: | 0.0004263 |
| inclination: | 97.7079° |
| perigee height: | 585 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 223.7604° |
| argument of perigee: | 83.4394° |
| revolutions per day: | 14.93150613 |
| mean anomaly at epoch: | 276.7311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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