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 44782U 26145.61950869 +.00000000 +00000-0 -77395-4 0 00006
2 44782 45.0086 280.6794 0012407 15.1596 344.9608 14.02066394 06
| Epoch (UTC): | 25 May 2026 14:52:05 |
| Eccentricity: | 0.0012407 |
| inclination: | 45.0086° |
| perigee height: | 878 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 280.6794° |
| argument of perigee: | 15.1596° |
| revolutions per day: | 14.02066394 |
| mean anomaly at epoch: | 344.9608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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