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 26019.67306802 +.00000000 +00000-0 -61231-4 0 00007
2 40921 82.4879 170.6805 0013536 349.9365 10.1442 12.42908275 02
| Epoch (UTC): | 19 January 2026 16:09:13 |
| Eccentricity: | 0.0013536 |
| inclination: | 82.4879° |
| perigee height: | 1484 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 170.6805° |
| argument of perigee: | 349.9365° |
| revolutions per day: | 12.42908275 |
| mean anomaly at epoch: | 10.1442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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