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 00053U 60009E 23030.83025412 -.00000019 00000-0 65844-3 0 9997
2 00053 47.2738 186.5092 0098966 31.3966 329.2682 12.17289124785186
| Epoch (UTC): | 30 January 2023 19:55:33 |
| Eccentricity: | 0.0098966 |
| inclination: | 47.2738° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 186.5092° |
| argument of perigee: | 31.3966° |
| revolutions per day: | 12.17289124 |
| mean anomaly at epoch: | 329.2682° |
| orbit number at epoch: | 78518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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