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 16229U 85028E 24357.72478409 .00005424 00000-0 18973-2 0 9990
2 16229 26.9056 207.3238 4727248 145.0304 257.9309 6.00139842677239
| Epoch (UTC): | 22 December 2024 17:23:41 |
| Eccentricity: | 0.4727248 |
| inclination: | 26.9056° |
| perigee height: | 366 km |
| apogee height: | 12459 km |
| right ascension of ascending node: | 207.3238° |
| argument of perigee: | 145.0304° |
| revolutions per day: | 6.00139842 |
| mean anomaly at epoch: | 257.9309° |
| orbit number at epoch: | 67723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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