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 47692U 26088.22793300 +.00000000 +00000-0 +15417-3 0 00002
2 47692 63.4059 55.0523 0164287 0.6746 359.4471 13.44209732 06
| Epoch (UTC): | 29 March 2026 05:28:13 |
| Eccentricity: | 0.0164287 |
| inclination: | 63.4059° |
| perigee height: | 971 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 55.0523° |
| argument of perigee: | 0.6746° |
| revolutions per day: | 13.44209732 |
| mean anomaly at epoch: | 359.4471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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