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 17732U 26088.10756633 +.00000000 +00000-0 +12155-2 0 00004
2 17732 65.8047 133.3412 0174446 258.9942 99.1469 13.99824325 08
| Epoch (UTC): | 29 March 2026 02:34:53 |
| Eccentricity: | 0.0174446 |
| inclination: | 65.8047° |
| perigee height: | 768 km |
| apogee height: | 1021 km |
| right ascension of ascending node: | 133.3412° |
| argument of perigee: | 258.9942° |
| revolutions per day: | 13.99824325 |
| mean anomaly at epoch: | 99.1469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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