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 29048U 06011B 21016.83429302 .00000090 00000-0 51690-4 0 9996
2 29048 71.9675 305.1156 0043222 9.4735 350.7207 14.28747543774278
| Epoch (UTC): | 16 January 2021 20:01:22 |
| Eccentricity: | 0.0043222 |
| inclination: | 71.9675° |
| perigee height: | 765 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 305.1156° |
| argument of perigee: | 9.4735° |
| revolutions per day: | 14.28747543 |
| mean anomaly at epoch: | 350.7207° |
| orbit number at epoch: | 77427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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