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 21023.17878156 -.00000123 00000-0 12797-4 0 9997
2 29 48.3810 351.6362 0023398 92.4203 267.9388 14.74399388251083
| Epoch (UTC): | 23 January 2021 04:17:26 |
| Eccentricity: | 0.0023398 |
| inclination: | 48.3810° |
| perigee height: | 630 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 351.6362° |
| argument of perigee: | 92.4203° |
| revolutions per day: | 14.74399388 |
| mean anomaly at epoch: | 267.9388° |
| orbit number at epoch: | 25108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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