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 6020U 72035B 23161.67620712 .00000048 00000-0 68850-4 0 9992
2 6020 74.0212 223.8472 0020009 68.7666 86.4204 13.78928917570263
| Epoch (UTC): | 10 June 2023 16:13:44 |
| Eccentricity: | 0.0020009 |
| inclination: | 74.0212° |
| perigee height: | 953 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 223.8472° |
| argument of perigee: | 68.7666° |
| revolutions per day: | 13.78928917 |
| mean anomaly at epoch: | 86.4204° |
| orbit number at epoch: | 57026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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