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 33749U 26145.57058749 +.00000000 +00000-0 +00000-0 0 00002
2 33749 1.2055 82.8576 0002218 329.3846 219.3883 1.00270755 06
| Epoch (UTC): | 25 May 2026 13:41:38 |
| Eccentricity: | 0.0002218 |
| inclination: | 1.2055° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 82.8576° |
| argument of perigee: | 329.3846° |
| revolutions per day: | 1.00270755 |
| mean anomaly at epoch: | 219.3883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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