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 68996U 26145.27557166 +.00000000 +00000-0 +20518-3 0 00007
2 68996 97.7384 43.1392 0003141 204.3207 155.7863 14.91176060 07
| Epoch (UTC): | 25 May 2026 06:36:49 |
| Eccentricity: | 0.0003141 |
| inclination: | 97.7384° |
| perigee height: | 592 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 43.1392° |
| argument of perigee: | 204.3207° |
| revolutions per day: | 14.91176060 |
| mean anomaly at epoch: | 155.7863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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