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 24720U 26150.05878169 +.00000000 +00000-0 +24808-2 0 00000
2 24720 31.2611 285.6882 5986296 206.7536 81.7384 3.84818971 04
| Epoch (UTC): | 30 May 2026 01:24:38 |
| Eccentricity: | 0.5986296 |
| inclination: | 31.2611° |
| perigee height: | 526 km |
| apogee height: | 21121 km |
| right ascension of ascending node: | 285.6882° |
| argument of perigee: | 206.7536° |
| revolutions per day: | 3.84818971 |
| mean anomaly at epoch: | 81.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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