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 44506U 26145.46236689 +.00000000 +00000-0 +00000-0 0 00004
2 44506 55.6478 332.0448 0060845 197.3305 341.1961 2.00569601 05
| Epoch (UTC): | 25 May 2026 11:05:48 |
| Eccentricity: | 0.0060845 |
| inclination: | 55.6478° |
| perigee height: | 20020 km |
| apogee height: | 20343 km |
| right ascension of ascending node: | 332.0448° |
| argument of perigee: | 197.3305° |
| revolutions per day: | 2.00569601 |
| mean anomaly at epoch: | 341.1961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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