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 69082U 26145.61275627 +.00000000 +00000-0 +31673-4 0 00006
2 69082 88.9867 344.1986 0003413 172.3236 187.8006 14.19911211 03
| Epoch (UTC): | 25 May 2026 14:42:22 |
| Eccentricity: | 0.0003413 |
| inclination: | 88.9867° |
| perigee height: | 823 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 344.1986° |
| argument of perigee: | 172.3236° |
| revolutions per day: | 14.19911211 |
| mean anomaly at epoch: | 187.8006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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