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 69033U 26145.58335647 +.00000000 +00000-0 -18031-1 0 00008
2 69033 97.2846 0.3597 0001434 89.8109 226.9968 15.70231244 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001434 |
| inclination: | 97.2846° |
| perigee height: | 357 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 0.3597° |
| argument of perigee: | 89.8109° |
| revolutions per day: | 15.70231244 |
| mean anomaly at epoch: | 226.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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