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 33436U 26145.51626507 +.00000000 +00000-0 +00000-0 0 00002
2 33436 0.2399 81.9629 0004872 13.6748 352.7435 1.00275888 07
| Epoch (UTC): | 25 May 2026 12:23:25 |
| Eccentricity: | 0.0004872 |
| inclination: | 0.2399° |
| perigee height: | 35765 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 81.9629° |
| argument of perigee: | 13.6748° |
| revolutions per day: | 1.00275888 |
| mean anomaly at epoch: | 352.7435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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