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 22803U 26088.09846565 +.00000000 +00000-0 -69569-4 0 00005
2 22803 70.9918 330.2002 0017394 188.3592 171.7245 14.17234899 06
| Epoch (UTC): | 29 March 2026 02:21:47 |
| Eccentricity: | 0.0017394 |
| inclination: | 70.9918° |
| perigee height: | 822 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 330.2002° |
| argument of perigee: | 188.3592° |
| revolutions per day: | 14.17234899 |
| mean anomaly at epoch: | 171.7245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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