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 43803U 26110.64391580 +.00000000 +00000-0 +44453-3 0 00000
2 43803 97.4170 173.3478 0007500 114.5830 245.6194 15.31804037 08
| Epoch (UTC): | 20 April 2026 15:27:14 |
| Eccentricity: | 0.0007500 |
| inclination: | 97.4170° |
| perigee height: | 465 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 173.3478° |
| argument of perigee: | 114.5830° |
| revolutions per day: | 15.31804037 |
| mean anomaly at epoch: | 245.6194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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