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 26040.54007747 +.00000000 +00000-0 +76057-4 0 00004
2 08459 74.0591 70.6981 0015363 173.9252 186.2091 14.38189484 09
| Epoch (UTC): | 09 February 2026 12:57:42 |
| Eccentricity: | 0.0015363 |
| inclination: | 74.0591° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 70.6981° |
| argument of perigee: | 173.9252° |
| revolutions per day: | 14.38189484 |
| mean anomaly at epoch: | 186.2091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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