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 29275U 06033D 24357.29642290 .00002630 00000-0 13499-2 0 9991
2 29275 6.3912 2.6080 7000706 342.0064 2.2355 2.61807365163031
| Epoch (UTC): | 22 December 2024 07:06:50 |
| Eccentricity: | 0.7000706 |
| inclination: | 6.3912° |
| perigee height: | 291 km |
| apogee height: | 31426 km |
| right ascension of ascending node: | 2.6080° |
| argument of perigee: | 342.0064° |
| revolutions per day: | 2.61807365 |
| mean anomaly at epoch: | 2.2355° |
| orbit number at epoch: | 16303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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