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 24883U 26088.00407427 +.00000000 +00000-0 +12972-3 0 00000
2 24883 98.8602 252.8311 0002396 29.9561 330.1760 14.35508307 00
| Epoch (UTC): | 29 March 2026 00:05:52 |
| Eccentricity: | 0.0002396 |
| inclination: | 98.8602° |
| perigee height: | 772 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 252.8311° |
| argument of perigee: | 29.9561° |
| revolutions per day: | 14.35508307 |
| mean anomaly at epoch: | 330.1760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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