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 26104.01879007 +.00000000 +00000-0 +41300-4 0 00005
2 06153 35.0050 96.0228 0006018 90.2290 307.3661 14.60025368 05
| Epoch (UTC): | 14 April 2026 00:27:03 |
| Eccentricity: | 0.0006018 |
| inclination: | 35.0050° |
| perigee height: | 689 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 96.0228° |
| argument of perigee: | 90.2290° |
| revolutions per day: | 14.60025368 |
| mean anomaly at epoch: | 307.3661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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