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 29236U 26145.56414168 +.00000000 +00000-0 +00000-0 0 00008
2 29236 0.0637 105.6492 0002659 315.7200 285.8782 1.00272229 02
| Epoch (UTC): | 25 May 2026 13:32:21 |
| Eccentricity: | 0.0002659 |
| inclination: | 0.0637° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 105.6492° |
| argument of perigee: | 315.7200° |
| revolutions per day: | 1.00272229 |
| mean anomaly at epoch: | 285.8782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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