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 20578U 26068.37905536 +.00000000 +00000-0 +63901-4 0 00008
2 20578 82.9468 153.4693 0014090 67.9461 3.9419 13.76636616 00
| Epoch (UTC): | 09 March 2026 09:05:50 |
| Eccentricity: | 0.0014090 |
| inclination: | 82.9468° |
| perigee height: | 965 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 153.4693° |
| argument of perigee: | 67.9461° |
| revolutions per day: | 13.76636616 |
| mean anomaly at epoch: | 3.9419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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