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 data is extracted from the following two-line orbital elements,
1 32295U 07056C 24357.47534843 .00006935 00000-0 99722-3 0 9993
2 32295 6.0714 123.7649 6803996 278.6254 15.4998 2.91634199158440
| Epoch (UTC): | 22 December 2024 11:24:30 |
| Eccentricity: | 0.6803996 |
| inclination: | 6.0714° |
| perigee height: | 235 km |
| apogee height: | 28395 km |
| right ascension of ascending node: | 123.7649° |
| argument of perigee: | 278.6254° |
| revolutions per day: | 2.91634199 |
| mean anomaly at epoch: | 15.4998° |
| orbit number at epoch: | 15844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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