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 20642U 90050E 23068.13220701 0.00005255 00000-0 50418-3 0 04
2 20642 63.3202 156.4228 0922954 59.8116 300.1368 13.45426883 06
| Epoch (UTC): | 09 March 2023 03:10:22 |
| Eccentricity: | 0.0922954 |
| inclination: | 63.3202° |
| perigee height: | 400 km |
| apogee height: | 1778 km |
| right ascension of ascending node: | 156.4228° |
| argument of perigee: | 59.8116° |
| revolutions per day: | 13.45426883 |
| mean anomaly at epoch: | 300.1368° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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