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 23029.84511007 -.00000034 00000-0 50701-3 0 9999
2 00053 47.2735 189.5475 0098999 28.4890 332.1263 12.17289007785065
| Epoch (UTC): | 29 January 2023 20:16:57 |
| Eccentricity: | 0.0098999 |
| inclination: | 47.2735° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 189.5475° |
| argument of perigee: | 28.4890° |
| revolutions per day: | 12.17289007 |
| mean anomaly at epoch: | 332.1263° |
| orbit number at epoch: | 78506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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