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 28480U 04046B 24283.84482335 .00000889 00000-0 34834-3 0 9992
2 28480 98.1713 220.4339 0139050 240.0345 118.6973 14.26560102 34944
| Epoch (UTC): | 09 October 2024 20:16:32 |
| Eccentricity: | 0.0139050 |
| inclination: | 98.1713° |
| perigee height: | 703 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 220.4339° |
| argument of perigee: | 240.0345° |
| revolutions per day: | 14.26560102 |
| mean anomaly at epoch: | 118.6973° |
| orbit number at epoch: | 3494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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