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 42834U 17042K 24358.14877581 .00008990 00000-0 70000-3 0 9994
2 42834 97.3766 171.1362 0011059 118.5139 241.7201 15.01398170405580
| Epoch (UTC): | 23 December 2024 03:34:14 |
| Eccentricity: | 0.0011059 |
| inclination: | 97.3766° |
| perigee height: | 555 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 171.1362° |
| argument of perigee: | 118.5139° |
| revolutions per day: | 15.01398170 |
| mean anomaly at epoch: | 241.7201° |
| orbit number at epoch: | 40558 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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