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 08459U 26041.44435770 +.00000000 +00000-0 +73131-4 0 00005
2 08459 74.0591 69.0344 0015329 172.0214 188.1187 14.38189862 01
| Epoch (UTC): | 10 February 2026 10:39:52 |
| Eccentricity: | 0.0015329 |
| inclination: | 74.0591° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 69.0344° |
| argument of perigee: | 172.0214° |
| revolutions per day: | 14.38189862 |
| mean anomaly at epoch: | 188.1187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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