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 69089U 26144.82336895 +.00000000 +00000-0 +27306-4 0 00008
2 69089 88.9868 344.2850 0003543 163.5392 196.5916 14.25359790 03
| Epoch (UTC): | 24 May 2026 19:45:39 |
| Eccentricity: | 0.0003543 |
| inclination: | 88.9868° |
| perigee height: | 805 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 344.2850° |
| argument of perigee: | 163.5392° |
| revolutions per day: | 14.25359790 |
| mean anomaly at epoch: | 196.5916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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