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 18153U 26157.04308029 +.00000000 +00000-0 +57574-4 0 00000
2 18153 82.4995 265.7338 0022160 82.2426 278.1305 14.85703079 06
| Epoch (UTC): | 06 June 2026 01:02:02 |
| Eccentricity: | 0.0022160 |
| inclination: | 82.4995° |
| perigee height: | 596 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 265.7338° |
| argument of perigee: | 82.2426° |
| revolutions per day: | 14.85703079 |
| mean anomaly at epoch: | 278.1305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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