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 26545U 00057A 23269.84408212 .00002793 00000-0 31794-3 0 9993
2 26545 64.5549 169.6988 0054452 264.0562 95.4338 14.87217440244830
| Epoch (UTC): | 26 September 2023 20:15:28 |
| Eccentricity: | 0.0054452 |
| inclination: | 64.5549° |
| perigee height: | 568 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 169.6988° |
| argument of perigee: | 264.0562° |
| revolutions per day: | 14.87217440 |
| mean anomaly at epoch: | 95.4338° |
| orbit number at epoch: | 24483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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