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 00051U 60009C 24280.84040050 .00000016 00000-0 97414-3 0 9993
2 00051 47.2115 162.6981 0106315 157.1075 203.4500 12.18336980855781
| Epoch (UTC): | 06 October 2024 20:10:10 |
| Eccentricity: | 0.0106315 |
| inclination: | 47.2115° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 162.6981° |
| argument of perigee: | 157.1075° |
| revolutions per day: | 12.18336980 |
| mean anomaly at epoch: | 203.4500° |
| orbit number at epoch: | 85578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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