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 26018.81225388 +.00000000 +00000-0 +73701-4 0 00002
2 26906 63.4207 183.4500 0615524 341.4274 16.5141 13.45125860 09
| Epoch (UTC): | 18 January 2026 19:29:38 |
| Eccentricity: | 0.0615524 |
| inclination: | 63.4207° |
| perigee height: | 631 km |
| apogee height: | 1550 km |
| right ascension of ascending node: | 183.4500° |
| argument of perigee: | 341.4274° |
| revolutions per day: | 13.45125860 |
| mean anomaly at epoch: | 16.5141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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