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 24278U 26101.47285316 +.00000000 +00000-0 +23606-4 0 00003
2 24278 98.5326 319.4497 0348803 269.5697 86.5475 13.53270999 08
| Epoch (UTC): | 11 April 2026 11:20:54 |
| Eccentricity: | 0.0348803 |
| inclination: | 98.5326° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 319.4497° |
| argument of perigee: | 269.5697° |
| revolutions per day: | 13.53270999 |
| mean anomaly at epoch: | 86.5475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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