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 48271U 21034D 24358.13457989 .00010270 00000-0 87018-3 0 9997
2 48271 97.6325 56.1019 0001396 6.3445 353.7795 14.98165728198580
| Epoch (UTC): | 23 December 2024 03:13:47 |
| Eccentricity: | 0.0001396 |
| inclination: | 97.6325° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 56.1019° |
| argument of perigee: | 6.3445° |
| revolutions per day: | 14.98165728 |
| mean anomaly at epoch: | 353.7795° |
| orbit number at epoch: | 19858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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