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 00051U 60009C 22146.45451173 -.00000023 00000-0 60505-3 0 9991
2 00051 47.2136 317.0422 0108433 108.1206 253.1426 12.18282761750404
| Epoch (UTC): | 26 May 2022 10:54:29 |
| Eccentricity: | 0.0108433 |
| inclination: | 47.2136° |
| perigee height: | 1513 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 317.0422° |
| argument of perigee: | 108.1206° |
| revolutions per day: | 12.18282761 |
| mean anomaly at epoch: | 253.1426° |
| orbit number at epoch: | 75040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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