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 29U 60002B 22019.04079074 .00000133 00000-0 50538-4 0 9996
2 29 48.3800 88.3833 0024276 197.8891 162.1168 14.74507550304339
| Epoch (UTC): | 19 January 2022 00:58:44 |
| Eccentricity: | 0.0024276 |
| inclination: | 48.3800° |
| perigee height: | 629 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 88.3833° |
| argument of perigee: | 197.8891° |
| revolutions per day: | 14.74507550 |
| mean anomaly at epoch: | 162.1168° |
| orbit number at epoch: | 30433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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