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 69079U 26145.62012817 +.00000000 +00000-0 +31791-4 0 00004
2 69079 88.9867 344.1998 0003166 171.3061 188.8184 14.19026246 05
| Epoch (UTC): | 25 May 2026 14:52:59 |
| Eccentricity: | 0.0003166 |
| inclination: | 88.9867° |
| perigee height: | 826 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 344.1998° |
| argument of perigee: | 171.3061° |
| revolutions per day: | 14.19026246 |
| mean anomaly at epoch: | 188.8184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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