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 55191U 26087.51661697 +.00000000 +00000-0 +36311-3 0 00005
2 55191 98.7215 101.3210 0047734 212.4942 147.3296 14.24218055 06
| Epoch (UTC): | 28 March 2026 12:23:55 |
| Eccentricity: | 0.0047734 |
| inclination: | 98.7215° |
| perigee height: | 777 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 101.3210° |
| argument of perigee: | 212.4942° |
| revolutions per day: | 14.24218055 |
| mean anomaly at epoch: | 147.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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