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 00050U 60009B 23029.28689802 -.00000105 00000-0 -19221-3 0 9995
2 00050 47.2334 34.6649 0114325 294.2642 64.6239 12.20126169786929
| Epoch (UTC): | 29 January 2023 06:53:07 |
| Eccentricity: | 0.0114325 |
| inclination: | 47.2334° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 34.6649° |
| argument of perigee: | 294.2642° |
| revolutions per day: | 12.20126169 |
| mean anomaly at epoch: | 64.6239° |
| orbit number at epoch: | 78692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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