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 24305U 26154.54080612 +.00000000 +00000-0 +70782-4 0 00009
2 24305 82.9367 90.3073 0028786 291.1569 68.6511 13.74083267 05
| Epoch (UTC): | 03 June 2026 12:58:45 |
| Eccentricity: | 0.0028786 |
| inclination: | 82.9367° |
| perigee height: | 964 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 90.3073° |
| argument of perigee: | 291.1569° |
| revolutions per day: | 13.74083267 |
| mean anomaly at epoch: | 68.6511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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