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 28479U 04046A 24358.12654787 .00002508 00000-0 47849-3 0 9996
2 28479 98.0703 6.9826 0010102 162.1616 197.9943 14.64805834 70638
| Epoch (UTC): | 23 December 2024 03:02:13 |
| Eccentricity: | 0.0010102 |
| inclination: | 98.0703° |
| perigee height: | 670 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 6.9826° |
| argument of perigee: | 162.1616° |
| revolutions per day: | 14.64805834 |
| mean anomaly at epoch: | 197.9943° |
| orbit number at epoch: | 7063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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