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 61160U 24140RE 24357.39478522 .00010063 00000-0 47250-2 0 9996
2 61160 88.9928 335.5018 0066608 171.4248 188.8097 14.18821174 17374
| Epoch (UTC): | 22 December 2024 09:28:29 |
| Eccentricity: | 0.0066608 |
| inclination: | 88.9928° |
| perigee height: | 781 km |
| apogee height: | 877 km |
| right ascension of ascending node: | 335.5018° |
| argument of perigee: | 171.4248° |
| revolutions per day: | 14.18821174 |
| mean anomaly at epoch: | 188.8097° |
| orbit number at epoch: | 1737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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