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 27717U 03013D 24278.66245954 -.00000150 00000-0 94890-3 0 9995
2 27717 1.6043 82.1436 7079859 303.6040 24.8872 2.22461982174712
| Epoch (UTC): | 04 October 2024 15:53:56 |
| Eccentricity: | 0.7079859 |
| inclination: | 1.6043° |
| perigee height: | 860 km |
| apogee height: | 35958 km |
| right ascension of ascending node: | 82.1436° |
| argument of perigee: | 303.6040° |
| revolutions per day: | 2.22461982 |
| mean anomaly at epoch: | 24.8872° |
| orbit number at epoch: | 17471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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