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 12442U 81041A 24357.88544241 .00000376 00000-0 14735-3 0 9993
2 12442 74.0540 273.4435 0011059 274.5047 85.4841 14.32866022278447
| Epoch (UTC): | 22 December 2024 21:15:02 |
| Eccentricity: | 0.0011059 |
| inclination: | 74.0540° |
| perigee height: | 774 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 273.4435° |
| argument of perigee: | 274.5047° |
| revolutions per day: | 14.32866022 |
| mean anomaly at epoch: | 85.4841° |
| orbit number at epoch: | 27844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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