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 69038U 26145.58335647 +.00000000 +00000-0 -24833-1 0 00000
2 69038 97.2848 0.3405 0002071 99.6927 165.5912 15.61124817 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002071 |
| inclination: | 97.2848° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 0.3405° |
| argument of perigee: | 99.6927° |
| revolutions per day: | 15.61124817 |
| mean anomaly at epoch: | 165.5912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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