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 29526U 26145.58901513 +.00000000 +00000-0 +00000-0 0 00007
2 29526 1.9489 81.3500 0004881 327.4283 72.8584 1.00276809 01
| Epoch (UTC): | 25 May 2026 14:08:10 |
| Eccentricity: | 0.0004881 |
| inclination: | 1.9489° |
| perigee height: | 35765 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 81.3500° |
| argument of perigee: | 327.4283° |
| revolutions per day: | 1.00276809 |
| mean anomaly at epoch: | 72.8584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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