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 23026.05912130 -.00000034 00000-0 49889-3 0 9994
2 00051 47.2121 280.2875 0107242 114.0751 247.1300 12.18291614780223
| Epoch (UTC): | 26 January 2023 01:25:08 |
| Eccentricity: | 0.0107242 |
| inclination: | 47.2121° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 280.2875° |
| argument of perigee: | 114.0751° |
| revolutions per day: | 12.18291614 |
| mean anomaly at epoch: | 247.1300° |
| orbit number at epoch: | 78022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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