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 42759U 17034B 23033.54013984 .00007599 00000-0 41881-3 0 9992
2 42759 43.0160 142.5882 0011840 307.2142 164.4016 15.14318759311209
| Epoch (UTC): | 02 February 2023 12:57:48 |
| Eccentricity: | 0.0011840 |
| inclination: | 43.0160° |
| perigee height: | 515 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 142.5882° |
| argument of perigee: | 307.2142° |
| revolutions per day: | 15.14318759 |
| mean anomaly at epoch: | 164.4016° |
| orbit number at epoch: | 31120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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