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 33504U 26107.91227683 +.00000000 +00000-0 +20157-3 0 00000
2 33504 82.4305 235.0637 0010495 20.0256 340.1401 15.44388492 00
| Epoch (UTC): | 17 April 2026 21:53:40 |
| Eccentricity: | 0.0010495 |
| inclination: | 82.4305° |
| perigee height: | 426 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 235.0637° |
| argument of perigee: | 20.0256° |
| revolutions per day: | 15.44388492 |
| mean anomaly at epoch: | 340.1401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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