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 69090U 26145.45667198 +.00000000 +00000-0 +34157-4 0 00005
2 69090 88.9868 344.2125 0002825 153.2178 206.9161 14.24071791 09
| Epoch (UTC): | 25 May 2026 10:57:36 |
| Eccentricity: | 0.0002825 |
| inclination: | 88.9868° |
| perigee height: | 810 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 344.2125° |
| argument of perigee: | 153.2178° |
| revolutions per day: | 14.24071791 |
| mean anomaly at epoch: | 206.9161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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