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 20528U 26159.14374123 +.00000000 +00000-0 +47455-5 0 00008
2 20528 82.9350 161.2898 0030321 275.1931 157.7456 13.73149245 02
| Epoch (UTC): | 08 June 2026 03:26:59 |
| Eccentricity: | 0.0030321 |
| inclination: | 82.9350° |
| perigee height: | 966 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 161.2898° |
| argument of perigee: | 275.1931° |
| revolutions per day: | 13.73149245 |
| mean anomaly at epoch: | 157.7456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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