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 62708U 26145.21218978 +.00000000 +00000-0 +25524-3 0 00003
2 62708 97.7082 225.7803 0000381 82.7362 277.3903 14.97616598 02
| Epoch (UTC): | 25 May 2026 05:05:33 |
| Eccentricity: | 0.0000381 |
| inclination: | 97.7082° |
| perigee height: | 574 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 225.7803° |
| argument of perigee: | 82.7362° |
| revolutions per day: | 14.97616598 |
| mean anomaly at epoch: | 277.3903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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