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 22207U 26110.96687144 +.00000000 +00000-0 +51841-4 0 00004
2 22207 82.9239 177.9234 0033236 157.7477 15.1417 13.73088177 00
| Epoch (UTC): | 20 April 2026 23:12:17 |
| Eccentricity: | 0.0033236 |
| inclination: | 82.9239° |
| perigee height: | 964 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 177.9234° |
| argument of perigee: | 157.7477° |
| revolutions per day: | 13.73088177 |
| mean anomaly at epoch: | 15.1417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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