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 42775U 17036L 24245.29764800 .13343114 24078-5 23541-3 0 9999
2 42775 97.0675 277.5924 0011337 248.5174 111.4922 16.47090026401159
| Epoch (UTC): | 01 September 2024 07:08:36 |
| Eccentricity: | 0.0011337 |
| inclination: | 97.0675° |
| perigee height: | 139 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 277.5924° |
| argument of perigee: | 248.5174° |
| revolutions per day: | 16.47090026 |
| mean anomaly at epoch: | 111.4922° |
| orbit number at epoch: | 40115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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