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 20855U 90081T 23033.51513366 .00000178 00000-0 12757-3 0 9990
2 20855 98.7173 32.1269 0024308 14.2904 97.5416 14.08763735666001
| Epoch (UTC): | 02 February 2023 12:21:47 |
| Eccentricity: | 0.0024308 |
| inclination: | 98.7173° |
| perigee height: | 846 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 32.1269° |
| argument of perigee: | 14.2904° |
| revolutions per day: | 14.08763735 |
| mean anomaly at epoch: | 97.5416° |
| orbit number at epoch: | 66600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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