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 36033U 26145.58355509 +.00000000 +00000-0 +00000-0 0 00006
2 36033 0.0508 117.3348 0001909 313.4980 21.5660 1.00272480 08
| Epoch (UTC): | 25 May 2026 14:00:19 |
| Eccentricity: | 0.0001909 |
| inclination: | 0.0508° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 117.3348° |
| argument of perigee: | 313.4980° |
| revolutions per day: | 1.00272480 |
| mean anomaly at epoch: | 21.5660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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