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 10654U 26074.76941686 +.00000000 +00000-0 +52755-2 0 00001
2 10654 102.4888 17.3129 0196135 51.5522 338.5060 12.95374827 00
| Epoch (UTC): | 15 March 2026 18:27:57 |
| Eccentricity: | 0.0196135 |
| inclination: | 102.4888° |
| perigee height: | 1130 km |
| apogee height: | 1430 km |
| right ascension of ascending node: | 17.3129° |
| argument of perigee: | 51.5522° |
| revolutions per day: | 12.95374827 |
| mean anomaly at epoch: | 338.5060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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