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 62705U 26145.19481622 +.00000000 +00000-0 +69330-3 0 00008
2 62705 97.8252 231.7120 0001094 92.6146 267.5203 15.00866269 01
| Epoch (UTC): | 25 May 2026 04:40:32 |
| Eccentricity: | 0.0001094 |
| inclination: | 97.8252° |
| perigee height: | 563 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 231.7120° |
| argument of perigee: | 92.6146° |
| revolutions per day: | 15.00866269 |
| mean anomaly at epoch: | 267.5203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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