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 33459U 26145.50248500 +.00000000 +00000-0 +00000-0 0 00009
2 33459 2.8944 79.4507 0004083 345.8580 308.3704 1.00269809 03
| Epoch (UTC): | 25 May 2026 12:03:34 |
| Eccentricity: | 0.0004083 |
| inclination: | 2.8944° |
| perigee height: | 35770 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 79.4507° |
| argument of perigee: | 345.8580° |
| revolutions per day: | 1.00269809 |
| mean anomaly at epoch: | 308.3704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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