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 69086U 26145.25153006 +.00000000 +00000-0 +32742-4 0 00004
2 69086 88.9865 344.2387 0002817 172.2791 187.8444 14.22142742 08
| Epoch (UTC): | 25 May 2026 06:02:12 |
| Eccentricity: | 0.0002817 |
| inclination: | 88.9865° |
| perigee height: | 816 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 344.2387° |
| argument of perigee: | 172.2791° |
| revolutions per day: | 14.22142742 |
| mean anomaly at epoch: | 187.8444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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