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 39430U 13066Q 24261.14755995 .00013143 00000-0 21356-2 0 9996
2 39430 97.7171 129.9461 0137070 320.8955 38.2403 14.65108136576503
| Epoch (UTC): | 17 September 2024 03:32:29 |
| Eccentricity: | 0.0137070 |
| inclination: | 97.7171° |
| perigee height: | 580 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 129.9461° |
| argument of perigee: | 320.8955° |
| revolutions per day: | 14.65108136 |
| mean anomaly at epoch: | 38.2403° |
| orbit number at epoch: | 57650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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