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 62033U 26145.44684583 +.00000000 +00000-0 +55242-3 0 00008
2 62033 43.0040 189.8520 0002112 269.2328 90.8282 15.27555009 06
| Epoch (UTC): | 25 May 2026 10:43:27 |
| Eccentricity: | 0.0002112 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 189.8520° |
| argument of perigee: | 269.2328° |
| revolutions per day: | 15.27555009 |
| mean anomaly at epoch: | 90.8282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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