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 26070.04463808 +.00000000 +00000-0 +69094-3 0 00003
2 29271 49.5535 17.5018 5182846 202.5622 122.4597 5.32994699 05
| Epoch (UTC): | 11 March 2026 01:04:16 |
| Eccentricity: | 0.5182846 |
| inclination: | 49.5535° |
| perigee height: | 291 km |
| apogee height: | 14641 km |
| right ascension of ascending node: | 17.5018° |
| argument of perigee: | 202.5622° |
| revolutions per day: | 5.32994699 |
| mean anomaly at epoch: | 122.4597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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