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 26072.92573062 +.00000000 +00000-0 +40740-3 0 00005
2 24827 63.3114 5.6655 1089638 68.5114 355.7810 11.07980201 08
| Epoch (UTC): | 13 March 2026 22:13:03 |
| Eccentricity: | 0.1089638 |
| inclination: | 63.3114° |
| perigee height: | 1195 km |
| apogee height: | 3047 km |
| right ascension of ascending node: | 5.6655° |
| argument of perigee: | 68.5114° |
| revolutions per day: | 11.07980201 |
| mean anomaly at epoch: | 355.7810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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