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 43486U 18048C 24277.83938984 .00017795 00000-0 19688-2 0 9993
2 43486 97.6515 317.5044 0014431 72.8394 287.4402 14.87336679342505
| Epoch (UTC): | 03 October 2024 20:08:43 |
| Eccentricity: | 0.0014431 |
| inclination: | 97.6515° |
| perigee height: | 596 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 317.5044° |
| argument of perigee: | 72.8394° |
| revolutions per day: | 14.87336679 |
| mean anomaly at epoch: | 287.4402° |
| orbit number at epoch: | 34250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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