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 57165U 83103C 24280.66438976 .00001291 00000-0 45293-3 0 9993
2 57165 74.0490 60.4577 0022134 320.9705 38.9849 14.35912556569751
| Epoch (UTC): | 06 October 2024 15:56:43 |
| Eccentricity: | 0.0022134 |
| inclination: | 74.0490° |
| perigee height: | 756 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 60.4577° |
| argument of perigee: | 320.9705° |
| revolutions per day: | 14.35912556 |
| mean anomaly at epoch: | 38.9849° |
| orbit number at epoch: | 56975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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