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 69076U 26145.62279333 +.00000000 +00000-0 +32023-4 0 00008
2 69076 88.9868 344.2002 0003535 147.9604 212.1801 14.18732440 08
| Epoch (UTC): | 25 May 2026 14:56:49 |
| Eccentricity: | 0.0003535 |
| inclination: | 88.9868° |
| perigee height: | 827 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 344.2002° |
| argument of perigee: | 147.9604° |
| revolutions per day: | 14.18732440 |
| mean anomaly at epoch: | 212.1801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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