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 26016.73066316 +.00000000 +00000-0 +64901-4 0 00007
2 26906 63.4207 188.8305 0615339 341.4240 16.5178 13.45125195 09
| Epoch (UTC): | 16 January 2026 17:32:09 |
| Eccentricity: | 0.0615339 |
| inclination: | 63.4207° |
| perigee height: | 631 km |
| apogee height: | 1550 km |
| right ascension of ascending node: | 188.8305° |
| argument of perigee: | 341.4240° |
| revolutions per day: | 13.45125195 |
| mean anomaly at epoch: | 16.5178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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