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 68907U 26145.53584543 +.00000000 +00000-0 +92777-3 0 00003
2 68907 97.2845 341.2030 0003248 82.8197 277.3423 15.49244693 07
| Epoch (UTC): | 25 May 2026 12:51:37 |
| Eccentricity: | 0.0003248 |
| inclination: | 97.2845° |
| perigee height: | 417 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 341.2030° |
| argument of perigee: | 82.8197° |
| revolutions per day: | 15.49244693 |
| mean anomaly at epoch: | 277.3423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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