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 26073.40705991 +.00000000 +00000-0 +53931-4 0 00007
2 44909 82.5211 42.6787 0217725 6.3050 354.0711 12.79747576 05
| Epoch (UTC): | 14 March 2026 09:46:09 |
| Eccentricity: | 0.0217725 |
| inclination: | 82.5211° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 42.6787° |
| argument of perigee: | 6.3050° |
| revolutions per day: | 12.79747576 |
| mean anomaly at epoch: | 354.0711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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