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 43941U 19004A 24339.66928064 0.00014000 00000-0 21337-3 0 04
2 43941 73.5870 297.2342 0015204 98.8119 261.1880 15.54217555 06
| Epoch (UTC): | 04 December 2024 16:03:45 |
| Eccentricity: | 0.0015204 |
| inclination: | 73.5870° |
| perigee height: | 394 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 297.2342° |
| argument of perigee: | 98.8119° |
| revolutions per day: | 15.54217555 |
| mean anomaly at epoch: | 261.1880° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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