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 26105.42632432 +.00000000 +00000-0 +51685-4 0 00007
2 24298 70.7583 97.4808 0012645 85.6327 274.6237 14.12425351 01
| Epoch (UTC): | 15 April 2026 10:13:54 |
| Eccentricity: | 0.0012645 |
| inclination: | 70.7583° |
| perigee height: | 842 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 97.4808° |
| argument of perigee: | 85.6327° |
| revolutions per day: | 14.12425351 |
| mean anomaly at epoch: | 274.6237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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