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 34885U 93036ACY 24357.84233296 .00006071 00000-0 16192-2 0 9992
2 34885 74.0328 129.8537 0016786 304.5030 180.7742 14.48548121823349
| Epoch (UTC): | 22 December 2024 20:12:57 |
| Eccentricity: | 0.0016786 |
| inclination: | 74.0328° |
| perigee height: | 718 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 129.8537° |
| argument of perigee: | 304.5030° |
| revolutions per day: | 14.48548121 |
| mean anomaly at epoch: | 180.7742° |
| orbit number at epoch: | 82334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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