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 26071.37442132 +.00000000 +00000-0 +10856-3 0 00004
2 44909 82.5207 44.0296 0217820 11.0528 349.5247 12.79747496 04
| Epoch (UTC): | 12 March 2026 08:59:10 |
| Eccentricity: | 0.0217820 |
| inclination: | 82.5207° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 44.0296° |
| argument of perigee: | 11.0528° |
| revolutions per day: | 12.79747496 |
| mean anomaly at epoch: | 349.5247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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