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 33056U 26145.52077176 +.00000000 +00000-0 +00000-0 0 00003
2 33056 0.0814 84.9751 0005159 332.9003 54.6956 1.00273408 06
| Epoch (UTC): | 25 May 2026 12:29:54 |
| Eccentricity: | 0.0005159 |
| inclination: | 0.0814° |
| perigee height: | 35764 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 84.9751° |
| argument of perigee: | 332.9003° |
| revolutions per day: | 1.00273408 |
| mean anomaly at epoch: | 54.6956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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