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 17528U 26064.30104642 +.00000000 +00000-0 +29346-3 0 00001
2 17528 97.4035 70.3453 0145020 27.5361 333.3426 14.54475002 07
| Epoch (UTC): | 05 March 2026 07:13:30 |
| Eccentricity: | 0.0145020 |
| inclination: | 97.4035° |
| perigee height: | 608 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 70.3453° |
| argument of perigee: | 27.5361° |
| revolutions per day: | 14.54475002 |
| mean anomaly at epoch: | 333.3426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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