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 22007U 26037.61985721 +.00000000 +00000-0 +10450-3 0 00004
2 22007 82.9313 107.5535 0031656 111.3639 249.0902 13.78262424 05
| Epoch (UTC): | 06 February 2026 14:52:35 |
| Eccentricity: | 0.0031656 |
| inclination: | 82.9313° |
| perigee height: | 947 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 107.5535° |
| argument of perigee: | 111.3639° |
| revolutions per day: | 13.78262424 |
| mean anomaly at epoch: | 249.0902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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