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 24827U 26064.64613355 +.00000000 +00000-0 +47584-3 0 00008
2 24827 63.3105 19.5544 1089378 68.4098 90.7108 11.07979498 02
| Epoch (UTC): | 05 March 2026 15:30:25 |
| Eccentricity: | 0.1089378 |
| inclination: | 63.3105° |
| perigee height: | 1195 km |
| apogee height: | 3047 km |
| right ascension of ascending node: | 19.5544° |
| argument of perigee: | 68.4098° |
| revolutions per day: | 11.07979498 |
| mean anomaly at epoch: | 90.7108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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