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 37169U 10048B 23159.52428680 .00014326 00000-0 34622-3 0 9990
2 37169 97.9947 6.2039 0005277 61.4880 298.6895 15.41275231706079
| Epoch (UTC): | 08 June 2023 12:34:58 |
| Eccentricity: | 0.0005277 |
| inclination: | 97.9947° |
| perigee height: | 439 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 6.2039° |
| argument of perigee: | 61.4880° |
| revolutions per day: | 15.41275231 |
| mean anomaly at epoch: | 298.6895° |
| orbit number at epoch: | 70607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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