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 26103.87840797 +.00000000 +00000-0 +41122-4 0 00001
2 24277 98.8064 157.5093 0000507 2.1939 357.9245 14.30380275 03
| Epoch (UTC): | 13 April 2026 21:04:54 |
| Eccentricity: | 0.0000507 |
| inclination: | 98.8064° |
| perigee height: | 790 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 157.5093° |
| argument of perigee: | 2.1939° |
| revolutions per day: | 14.30380275 |
| mean anomaly at epoch: | 357.9245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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