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 26088.18827838 +.00000000 +00000-0 +95432-4 0 00005
2 08459 74.0628 343.0467 0014557 68.2404 292.0298 14.38214966 04
| Epoch (UTC): | 29 March 2026 04:31:07 |
| Eccentricity: | 0.0014557 |
| inclination: | 74.0628° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 343.0467° |
| argument of perigee: | 68.2404° |
| revolutions per day: | 14.38214966 |
| mean anomaly at epoch: | 292.0298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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