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 26074.27102718 +.00000000 +00000-0 +30383-3 0 00003
2 26906 63.4224 40.0826 0620101 341.5721 16.3704 13.45172030 06
| Epoch (UTC): | 15 March 2026 06:30:16 |
| Eccentricity: | 0.0620101 |
| inclination: | 63.4224° |
| perigee height: | 627 km |
| apogee height: | 1553 km |
| right ascension of ascending node: | 40.0826° |
| argument of perigee: | 341.5721° |
| revolutions per day: | 13.45172030 |
| mean anomaly at epoch: | 16.3704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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