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 24920U 26108.69254856 +.00000000 +00000-0 +65599-4 0 00000
2 24920 69.9519 148.4021 0022149 351.7641 8.3115 14.27919119 05
| Epoch (UTC): | 18 April 2026 16:37:16 |
| Eccentricity: | 0.0022149 |
| inclination: | 69.9519° |
| perigee height: | 783 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 148.4021° |
| argument of perigee: | 351.7641° |
| revolutions per day: | 14.27919119 |
| mean anomaly at epoch: | 8.3115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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