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 22626U 26038.14548498 +.00000000 +00000-0 +23901-3 0 00001
2 22626 82.5193 295.9303 0017688 51.2919 308.9881 14.96422244 01
| Epoch (UTC): | 07 February 2026 03:29:29 |
| Eccentricity: | 0.0017688 |
| inclination: | 82.5193° |
| perigee height: | 566 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 295.9303° |
| argument of perigee: | 51.2919° |
| revolutions per day: | 14.96422244 |
| mean anomaly at epoch: | 308.9881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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