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 42065U 17011B 23267.82843158 0.00000000 00000-0 00000-0 0 09
2 42065 63.4419 168.8281 0082074 2.7689 357.2311 13.40902859 06
| Epoch (UTC): | 24 September 2023 19:52:56 |
| Eccentricity: | 0.0082074 |
| inclination: | 63.4419° |
| perigee height: | 1044 km |
| apogee height: | 1167 km |
| right ascension of ascending node: | 168.8281° |
| argument of perigee: | 2.7689° |
| revolutions per day: | 13.40902859 |
| mean anomaly at epoch: | 357.2311° |
| 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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