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 18412U 87041E 24358.18443682 .00000490 00000-0 47297-3 0 9999
2 18412 71.0285 37.0126 0194546 287.3049 70.6852 13.76674778888437
| Epoch (UTC): | 23 December 2024 04:25:35 |
| Eccentricity: | 0.0194546 |
| inclination: | 71.0285° |
| perigee height: | 832 km |
| apogee height: | 1119 km |
| right ascension of ascending node: | 37.0126° |
| argument of perigee: | 287.3049° |
| revolutions per day: | 13.76674778 |
| mean anomaly at epoch: | 70.6852° |
| orbit number at epoch: | 88843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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