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 68706U 26145.41242094 +.00000000 +00000-0 +10035-2 0 00005
2 68706 53.1594 38.8699 0001038 84.4177 275.6950 15.49330110 03
| Epoch (UTC): | 25 May 2026 09:53:53 |
| Eccentricity: | 0.0001038 |
| inclination: | 53.1594° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 38.8699° |
| argument of perigee: | 84.4177° |
| revolutions per day: | 15.49330110 |
| mean anomaly at epoch: | 275.6950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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