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 26067.60313508 +.00000000 +00000-0 +28867-3 0 00007
2 17528 97.4037 73.2708 0144734 17.1613 343.4407 14.54483680 02
| Epoch (UTC): | 08 March 2026 14:28:30 |
| Eccentricity: | 0.0144734 |
| inclination: | 97.4037° |
| perigee height: | 608 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 73.2708° |
| argument of perigee: | 17.1613° |
| revolutions per day: | 14.54483680 |
| mean anomaly at epoch: | 343.4407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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