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 44880U 26145.61924684 +.00000000 +00000-0 +39515-3 0 00001
2 44880 97.7814 230.0654 0012389 126.0785 234.1585 14.95716030 08
| Epoch (UTC): | 25 May 2026 14:51:42 |
| Eccentricity: | 0.0012389 |
| inclination: | 97.7814° |
| perigee height: | 572 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 230.0654° |
| argument of perigee: | 126.0785° |
| revolutions per day: | 14.95716030 |
| mean anomaly at epoch: | 234.1585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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