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 19325U 26072.28570963 +.00000000 +00000-0 +66746-4 0 00003
2 19325 82.9548 170.7992 0032281 292.6445 76.1886 13.77909672 08
| Epoch (UTC): | 13 March 2026 06:51:25 |
| Eccentricity: | 0.0032281 |
| inclination: | 82.9548° |
| perigee height: | 948 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 170.7992° |
| argument of perigee: | 292.6445° |
| revolutions per day: | 13.77909672 |
| mean anomaly at epoch: | 76.1886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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