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 69036U 26145.58335647 +.00000000 +00000-0 -23567-1 0 00001
2 69036 97.2848 0.3428 0002001 97.6692 172.5468 15.62627242 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002001 |
| inclination: | 97.2848° |
| perigee height: | 379 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 0.3428° |
| argument of perigee: | 97.6692° |
| revolutions per day: | 15.62627242 |
| mean anomaly at epoch: | 172.5468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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