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 43675U 18084E 24358.41396675 .00043337 00000-0 22486-2 0 9993
2 43675 98.0388 161.6197 0008588 46.4920 313.7023 15.15967270335247
| Epoch (UTC): | 23 December 2024 09:56:06 |
| Eccentricity: | 0.0008588 |
| inclination: | 98.0388° |
| perigee height: | 512 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 161.6197° |
| argument of perigee: | 46.4920° |
| revolutions per day: | 15.15967270 |
| mean anomaly at epoch: | 313.7023° |
| orbit number at epoch: | 33524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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