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 26906U 26047.28526299 +.00000000 +00000-0 +16145-3 0 00008
2 26906 63.4210 109.8507 0617787 341.5016 16.4406 13.45141398 07
| Epoch (UTC): | 16 February 2026 06:50:46 |
| Eccentricity: | 0.0617787 |
| inclination: | 63.4210° |
| perigee height: | 629 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 109.8507° |
| argument of perigee: | 341.5016° |
| revolutions per day: | 13.45141398 |
| mean anomaly at epoch: | 16.4406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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