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 33505U 26127.80599591 +.00000000 +00000-0 +10706-3 0 00000
2 33505 82.3850 246.2185 0021525 166.6084 193.5726 15.18490931 02
| Epoch (UTC): | 07 May 2026 19:20:38 |
| Eccentricity: | 0.0021525 |
| inclination: | 82.3850° |
| perigee height: | 496 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 246.2185° |
| argument of perigee: | 166.6084° |
| revolutions per day: | 15.18490931 |
| mean anomaly at epoch: | 193.5726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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