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 06153U 26142.31475315 +.00000000 +00000-0 +38948-4 0 00008
2 06153 35.0056 237.8255 0006256 38.1022 1.4561 14.60044774 07
| Epoch (UTC): | 22 May 2026 07:33:14 |
| Eccentricity: | 0.0006256 |
| inclination: | 35.0056° |
| perigee height: | 689 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 237.8255° |
| argument of perigee: | 38.1022° |
| revolutions per day: | 14.60044774 |
| mean anomaly at epoch: | 1.4561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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