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 24277U 26160.11887632 +.00000000 +00000-0 +49761-4 0 00007
2 24277 98.8002 214.4200 0002249 114.8763 245.2653 14.30395374 07
| Epoch (UTC): | 09 June 2026 02:51:10 |
| Eccentricity: | 0.0002249 |
| inclination: | 98.8002° |
| perigee height: | 789 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 214.4200° |
| argument of perigee: | 114.8763° |
| revolutions per day: | 14.30395374 |
| mean anomaly at epoch: | 245.2653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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