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 44078U 26088.16259541 +.00000000 +00000-0 +22803-4 0 00002
2 44078 98.4736 147.3729 0019810 98.5353 261.8083 14.43635293 05
| Epoch (UTC): | 29 March 2026 03:54:08 |
| Eccentricity: | 0.0019810 |
| inclination: | 98.4736° |
| perigee height: | 732 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 147.3729° |
| argument of perigee: | 98.5353° |
| revolutions per day: | 14.43635293 |
| mean anomaly at epoch: | 261.8083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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