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 23160.70308915 -.00000061 00000-0 24757-3 0 9994
2 00053 47.2735 145.9700 0097697 53.0286 307.9399 12.17300733801002
| Epoch (UTC): | 09 June 2023 16:52:26 |
| Eccentricity: | 0.0097697 |
| inclination: | 47.2735° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 145.9700° |
| argument of perigee: | 53.0286° |
| revolutions per day: | 12.17300733 |
| mean anomaly at epoch: | 307.9399° |
| orbit number at epoch: | 80100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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