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 44909U 26145.33250234 +.00000000 +00000-0 +45398-4 0 00002
2 44909 82.5226 354.8951 0217138 197.5572 161.7941 12.79748351 02
| Epoch (UTC): | 25 May 2026 07:58:48 |
| Eccentricity: | 0.0217138 |
| inclination: | 82.5226° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 354.8951° |
| argument of perigee: | 197.5572° |
| revolutions per day: | 12.79748351 |
| mean anomaly at epoch: | 161.7941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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