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 26067.13436704 +.00000000 +00000-0 +49278-3 0 00008
2 26906 63.4212 58.5339 0619429 341.5446 16.3970 13.45163046 03
| Epoch (UTC): | 08 March 2026 03:13:29 |
| Eccentricity: | 0.0619429 |
| inclination: | 63.4212° |
| perigee height: | 628 km |
| apogee height: | 1553 km |
| right ascension of ascending node: | 58.5339° |
| argument of perigee: | 341.5446° |
| revolutions per day: | 13.45163046 |
| mean anomaly at epoch: | 16.3970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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