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 4256U 69082B 23333.80801904 .00000301 00000-0 24628-3 0 9995
2 4256 70.0083 162.9265 0020725 210.6851 149.3046 13.98671019760349
| Epoch (UTC): | 29 November 2023 19:23:32 |
| Eccentricity: | 0.0020725 |
| inclination: | 70.0083° |
| perigee height: | 883 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 162.9265° |
| argument of perigee: | 210.6851° |
| revolutions per day: | 13.98671019 |
| mean anomaly at epoch: | 149.3046° |
| orbit number at epoch: | 76034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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