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 26162.18656223 +.00000000 +00000-0 +36254-4 0 00001
2 24305 82.9372 84.6483 0028669 268.8323 90.9548 13.74084131 00
| Epoch (UTC): | 11 June 2026 04:28:38 |
| Eccentricity: | 0.0028669 |
| inclination: | 82.9372° |
| perigee height: | 964 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 84.6483° |
| argument of perigee: | 268.8323° |
| revolutions per day: | 13.74084131 |
| mean anomaly at epoch: | 90.9548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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