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 23091.69758976 -.00000051 00000-0 33114-3 0 9994
2 00050 47.2298 200.9581 0113641 120.7327 240.4712 12.20128186794542
| Epoch (UTC): | 01 April 2023 16:44:31 |
| Eccentricity: | 0.0113641 |
| inclination: | 47.2298° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 200.9581° |
| argument of perigee: | 120.7327° |
| revolutions per day: | 12.20128186 |
| mean anomaly at epoch: | 240.4712° |
| orbit number at epoch: | 79454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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