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 5050U 71020A 23343.18798770 -.00000078 00000-0 27207-5 0 9991
2 5050 65.8253 297.7708 0015595 255.0624 205.8207 13.72167050641849
| Epoch (UTC): | 09 December 2023 04:30:42 |
| Eccentricity: | 0.0015595 |
| inclination: | 65.8253° |
| perigee height: | 980 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 297.7708° |
| argument of perigee: | 255.0624° |
| revolutions per day: | 13.72167050 |
| mean anomaly at epoch: | 205.8207° |
| orbit number at epoch: | 64184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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