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 26145.58786178 +.00000000 +00000-0 +11659-2 0 00002
2 40922 82.4866 92.3527 0015837 88.6640 271.6254 12.42883469 01
| Epoch (UTC): | 25 May 2026 14:06:31 |
| Eccentricity: | 0.0015837 |
| inclination: | 82.4866° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 92.3527° |
| argument of perigee: | 88.6640° |
| revolutions per day: | 12.42883469 |
| mean anomaly at epoch: | 271.6254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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