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 29164U 06020C 22229.00031072 .00052936 00000-0 32494-2 0 9999
2 29164 6.8327 65.6296 4401108 323.6395 13.2374 6.71943197282484
| Epoch (UTC): | 17 August 2022 00:00:26 |
| Eccentricity: | 0.4401108 |
| inclination: | 6.8327° |
| perigee height: | 263 km |
| apogee height: | 10705 km |
| right ascension of ascending node: | 65.6296° |
| argument of perigee: | 323.6395° |
| revolutions per day: | 6.71943197 |
| mean anomaly at epoch: | 13.2374° |
| orbit number at epoch: | 28248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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