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 10732U 26088.19863447 +.00000000 +00000-0 +27847-4 0 00004
2 10732 82.9358 30.0266 0018203 297.3910 175.6334 13.75596307 07
| Epoch (UTC): | 29 March 2026 04:46:02 |
| Eccentricity: | 0.0018203 |
| inclination: | 82.9358° |
| perigee height: | 966 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 30.0266° |
| argument of perigee: | 297.3910° |
| revolutions per day: | 13.75596307 |
| mean anomaly at epoch: | 175.6334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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