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 26073.20454484 +.00000000 +00000-0 +41974-3 0 00003
2 24827 63.3113 5.1978 1089648 68.5148 27.8957 11.07980231 00
| Epoch (UTC): | 14 March 2026 04:54:32 |
| Eccentricity: | 0.1089648 |
| inclination: | 63.3113° |
| perigee height: | 1195 km |
| apogee height: | 3047 km |
| right ascension of ascending node: | 5.1978° |
| argument of perigee: | 68.5148° |
| revolutions per day: | 11.07980231 |
| mean anomaly at epoch: | 27.8957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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