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 40922U 26100.50930074 +.00000000 +00000-0 -45480-3 0 00002
2 40922 82.4845 120.4389 0014406 183.2111 176.8879 12.42881265 04
| Epoch (UTC): | 10 April 2026 12:13:23 |
| Eccentricity: | 0.0014406 |
| inclination: | 82.4845° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 120.4389° |
| argument of perigee: | 183.2111° |
| revolutions per day: | 12.42881265 |
| mean anomaly at epoch: | 176.8879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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