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 26063.10806437 +.00000000 +00000-0 +79308-3 0 00000
2 29271 49.5521 23.0688 5183179 197.8237 133.7092 5.32917649 08
| Epoch (UTC): | 04 March 2026 02:35:36 |
| Eccentricity: | 0.5183179 |
| inclination: | 49.5521° |
| perigee height: | 291 km |
| apogee height: | 14643 km |
| right ascension of ascending node: | 23.0688° |
| argument of perigee: | 197.8237° |
| revolutions per day: | 5.32917649 |
| mean anomaly at epoch: | 133.7092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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