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 26069.94210034 +.00000000 +00000-0 +25128-3 0 00003
2 17528 97.4037 75.3432 0144523 9.7980 350.5984 14.54489060 06
| Epoch (UTC): | 10 March 2026 22:36:37 |
| Eccentricity: | 0.0144523 |
| inclination: | 97.4037° |
| perigee height: | 609 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 75.3432° |
| argument of perigee: | 9.7980° |
| revolutions per day: | 14.54489060 |
| mean anomaly at epoch: | 350.5984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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