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 22627U 26020.57876116 +.00000000 +00000-0 +83435-4 0 00000
2 22627 82.5193 62.6075 0023747 136.2829 224.0271 14.80041832 08
| Epoch (UTC): | 20 January 2026 13:53:24 |
| Eccentricity: | 0.0023747 |
| inclination: | 82.5193° |
| perigee height: | 613 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 62.6075° |
| argument of perigee: | 136.2829° |
| revolutions per day: | 14.80041832 |
| mean anomaly at epoch: | 224.0271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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