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 43782U 26111.63826610 +.00000000 +00000-0 +32399-3 0 00009
2 43782 97.4111 165.9137 0011936 129.7991 230.4297 15.20942913 02
| Epoch (UTC): | 21 April 2026 15:19:06 |
| Eccentricity: | 0.0011936 |
| inclination: | 97.4111° |
| perigee height: | 495 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 165.9137° |
| argument of perigee: | 129.7991° |
| revolutions per day: | 15.20942913 |
| mean anomaly at epoch: | 230.4297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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