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 44906U 26145.61858096 +.00000000 +00000-0 +11372-2 0 00003
2 44906 82.5233 99.0890 0014078 222.8079 137.1905 12.42871013 08
| Epoch (UTC): | 25 May 2026 14:50:45 |
| Eccentricity: | 0.0014078 |
| inclination: | 82.5233° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 99.0890° |
| argument of perigee: | 222.8079° |
| revolutions per day: | 12.42871013 |
| mean anomaly at epoch: | 137.1905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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