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 68956U 26145.58335647 +.00000000 +00000-0 -22966-1 0 00003
2 68956 53.1589 268.0717 0001055 61.6813 41.5158 15.63529099 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001055 |
| inclination: | 53.1589° |
| perigee height: | 377 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 268.0717° |
| argument of perigee: | 61.6813° |
| revolutions per day: | 15.63529099 |
| mean anomaly at epoch: | 41.5158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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