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 23088.42149016 -.00000092 00000-0 -49148-4 0 9991
2 00050 47.2299 211.1262 0113664 110.9336 250.3661 12.20128052794140
| Epoch (UTC): | 29 March 2023 10:06:56 |
| Eccentricity: | 0.0113664 |
| inclination: | 47.2299° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 211.1262° |
| argument of perigee: | 110.9336° |
| revolutions per day: | 12.20128052 |
| mean anomaly at epoch: | 250.3661° |
| orbit number at epoch: | 79414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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