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 26107.01077522 +.00000000 +00000-0 +16551-2 0 00009
2 40921 82.4826 116.2911 0014680 152.0266 208.1606 12.42913027 04
| Epoch (UTC): | 17 April 2026 00:15:30 |
| Eccentricity: | 0.0014680 |
| inclination: | 82.4826° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 116.2911° |
| argument of perigee: | 152.0266° |
| revolutions per day: | 12.42913027 |
| mean anomaly at epoch: | 208.1606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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