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 24971U 26017.99073748 +.00000000 +00000-0 +69463-4 0 00001
2 24971 98.8327 8.7126 0051373 310.9651 48.7094 14.35435547 03
| Epoch (UTC): | 17 January 2026 23:46:39 |
| Eccentricity: | 0.0051373 |
| inclination: | 98.8327° |
| perigee height: | 737 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 8.7126° |
| argument of perigee: | 310.9651° |
| revolutions per day: | 14.35435547 |
| mean anomaly at epoch: | 48.7094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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