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 26042.12082154 +.00000000 +00000-0 +84591-4 0 00002
2 22007 82.9305 104.1953 0031727 99.2725 261.2023 13.78263297 01
| Epoch (UTC): | 11 February 2026 02:53:58 |
| Eccentricity: | 0.0031727 |
| inclination: | 82.9305° |
| perigee height: | 947 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 104.1953° |
| argument of perigee: | 99.2725° |
| revolutions per day: | 13.78263297 |
| mean anomaly at epoch: | 261.2023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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