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 00046U 60007B 24256.93556262 .00007235 00000-0 13976-2 0 9995
2 00046 66.6903 176.7409 0194517 54.1605 307.7400 14.52538234363633
| Epoch (UTC): | 12 September 2024 22:27:12 |
| Eccentricity: | 0.0194517 |
| inclination: | 66.6903° |
| perigee height: | 579 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 176.7409° |
| argument of perigee: | 54.1605° |
| revolutions per day: | 14.52538234 |
| mean anomaly at epoch: | 307.7400° |
| orbit number at epoch: | 36363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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