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 40921U 26053.88368594 +.00000000 +00000-0 +33835-3 0 00001
2 40921 82.4911 149.3839 0012968 270.7739 89.1855 12.42909633 06
| Epoch (UTC): | 22 February 2026 21:12:30 |
| Eccentricity: | 0.0012968 |
| inclination: | 82.4911° |
| perigee height: | 1484 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 149.3839° |
| argument of perigee: | 270.7739° |
| revolutions per day: | 12.42909633 |
| mean anomaly at epoch: | 89.1855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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