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 13033U 26053.68736561 +.00000000 +00000-0 +33393-4 0 00006
2 13033 82.9376 249.8284 0032942 146.3361 285.6328 13.73463073 09
| Epoch (UTC): | 22 February 2026 16:29:48 |
| Eccentricity: | 0.0032942 |
| inclination: | 82.9376° |
| perigee height: | 963 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 249.8284° |
| argument of perigee: | 146.3361° |
| revolutions per day: | 13.73463073 |
| mean anomaly at epoch: | 285.6328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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