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 26106.88630745 +.00000000 +00000-0 +36476-4 0 00001
2 24277 98.8060 160.5541 0000323 347.9243 12.1931 14.30380754 09
| Epoch (UTC): | 16 April 2026 21:16:16 |
| Eccentricity: | 0.0000323 |
| inclination: | 98.8060° |
| perigee height: | 790 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 160.5541° |
| argument of perigee: | 347.9243° |
| revolutions per day: | 14.30380754 |
| mean anomaly at epoch: | 12.1931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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