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 26067.65475044 +.00000000 +00000-0 +48155-3 0 00008
2 26906 63.4214 57.1885 0619485 341.5472 16.3945 13.45163748 08
| Epoch (UTC): | 08 March 2026 15:42:50 |
| Eccentricity: | 0.0619485 |
| inclination: | 63.4214° |
| perigee height: | 627 km |
| apogee height: | 1553 km |
| right ascension of ascending node: | 57.1885° |
| argument of perigee: | 341.5472° |
| revolutions per day: | 13.45163748 |
| mean anomaly at epoch: | 16.3945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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