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 27424U 26088.19531542 +.00000000 +00000-0 +25591-3 0 00001
2 27424 98.4206 55.9204 0001155 117.6858 331.7498 14.62021580 07
| Epoch (UTC): | 29 March 2026 04:41:15 |
| Eccentricity: | 0.0001155 |
| inclination: | 98.4206° |
| perigee height: | 686 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 55.9204° |
| argument of perigee: | 117.6858° |
| revolutions per day: | 14.62021580 |
| mean anomaly at epoch: | 331.7498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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