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 24298U 26088.21687279 +.00000000 +00000-0 +89820-4 0 00005
2 24298 70.7585 133.9094 0013491 116.4863 243.7642 14.12421249 03
| Epoch (UTC): | 29 March 2026 05:12:17 |
| Eccentricity: | 0.0013491 |
| inclination: | 70.7585° |
| perigee height: | 841 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 133.9094° |
| argument of perigee: | 116.4863° |
| revolutions per day: | 14.12421249 |
| mean anomaly at epoch: | 243.7642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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