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 48759U 02032CU 24355.00900681 .00038415 00000-0 51449-2 0 9999
2 48759 98.8272 13.5967 0035862 123.6198 236.8441 14.78839069196500
| Epoch (UTC): | 20 December 2024 00:12:58 |
| Eccentricity: | 0.0035862 |
| inclination: | 98.8272° |
| perigee height: | 608 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 13.5967° |
| argument of perigee: | 123.6198° |
| revolutions per day: | 14.78839069 |
| mean anomaly at epoch: | 236.8441° |
| orbit number at epoch: | 19650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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