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 23711U 95059B 23152.55578524 -.00000018 00000-0 49452-4 0 9994
2 23711 100.5954 172.0950 0368573 90.0660 22.6336 13.12761719321047
| Epoch (UTC): | 01 June 2023 13:20:19 |
| Eccentricity: | 0.0368573 |
| inclination: | 100.5954° |
| perigee height: | 933 km |
| apogee height: | 1492 km |
| right ascension of ascending node: | 172.0950° |
| argument of perigee: | 90.0660° |
| revolutions per day: | 13.12761719 |
| mean anomaly at epoch: | 22.6336° |
| orbit number at epoch: | 32104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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