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 26019.31459095 +.00000000 +00000-0 +11334-2 0 00004
2 24827 63.3062 95.6119 1088197 67.7986 356.0336 11.07973034 04
| Epoch (UTC): | 19 January 2026 07:33:00 |
| Eccentricity: | 0.1088197 |
| inclination: | 63.3062° |
| perigee height: | 1196 km |
| apogee height: | 3046 km |
| right ascension of ascending node: | 95.6119° |
| argument of perigee: | 67.7986° |
| revolutions per day: | 11.07973034 |
| mean anomaly at epoch: | 356.0336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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