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 62680U 26145.13266010 +.00000000 +00000-0 +13249-2 0 00003
2 62680 97.4012 226.9508 0006154 62.8139 297.3727 15.28966561 00
| Epoch (UTC): | 25 May 2026 03:11:01 |
| Eccentricity: | 0.0006154 |
| inclination: | 97.4012° |
| perigee height: | 475 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 226.9508° |
| argument of perigee: | 62.8139° |
| revolutions per day: | 15.28966561 |
| mean anomaly at epoch: | 297.3727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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