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 32473U 07042C 24258.80653985 .00009826 00000-0 20935-2 0 9993
2 32473 97.9894 280.5202 0099750 83.5455 277.7090 14.56035847885888
| Epoch (UTC): | 14 September 2024 19:21:25 |
| Eccentricity: | 0.0099750 |
| inclination: | 97.9894° |
| perigee height: | 635 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 280.5202° |
| argument of perigee: | 83.5455° |
| revolutions per day: | 14.56035847 |
| mean anomaly at epoch: | 277.7090° |
| orbit number at epoch: | 88588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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