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 29055U 26145.58754177 +.00000000 +00000-0 +00000-0 0 00006
2 29055 0.4174 83.1213 0003511 339.7676 50.8011 1.00273939 07
| Epoch (UTC): | 25 May 2026 14:06:03 |
| Eccentricity: | 0.0003511 |
| inclination: | 0.4174° |
| perigee height: | 35771 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 83.1213° |
| argument of perigee: | 339.7676° |
| revolutions per day: | 1.00273939 |
| mean anomaly at epoch: | 50.8011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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