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 26550U 26022.30014597 +.00000000 +00000-0 +14549-3 0 00008
2 26550 64.5653 344.0163 0504565 66.1640 299.1452 13.82035420 08
| Epoch (UTC): | 22 January 2026 07:12:12 |
| Eccentricity: | 0.0504565 |
| inclination: | 64.5653° |
| perigee height: | 587 km |
| apogee height: | 1327 km |
| right ascension of ascending node: | 344.0163° |
| argument of perigee: | 66.1640° |
| revolutions per day: | 13.82035420 |
| mean anomaly at epoch: | 299.1452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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