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 33595U 26145.58147508 +.00000000 +00000-0 +00000-0 0 00004
2 33595 3.4082 78.6632 0004141 337.6347 25.1926 1.00271163 05
| Epoch (UTC): | 25 May 2026 13:57:19 |
| Eccentricity: | 0.0004141 |
| inclination: | 3.4082° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 78.6632° |
| argument of perigee: | 337.6347° |
| revolutions per day: | 1.00271163 |
| mean anomaly at epoch: | 25.1926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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