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 29271U 26068.16995669 +.00000000 +00000-0 +92957-3 0 00002
2 29271 49.5529 19.0064 5182907 201.2821 125.4307 5.32972568 04
| Epoch (UTC): | 09 March 2026 04:04:44 |
| Eccentricity: | 0.5182907 |
| inclination: | 49.5529° |
| perigee height: | 291 km |
| apogee height: | 14641 km |
| right ascension of ascending node: | 19.0064° |
| argument of perigee: | 201.2821° |
| revolutions per day: | 5.32972568 |
| mean anomaly at epoch: | 125.4307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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