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 12150U 81006B 24282.72940749 .00000325 00000-0 40391-3 0 9994
2 12150 65.8197 287.1465 0057246 325.1206 34.6111 13.77355546196630
| Epoch (UTC): | 08 October 2024 17:30:20 |
| Eccentricity: | 0.0057246 |
| inclination: | 65.8197° |
| perigee height: | 931 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 287.1465° |
| argument of perigee: | 325.1206° |
| revolutions per day: | 13.77355546 |
| mean anomaly at epoch: | 34.6111° |
| orbit number at epoch: | 19663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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