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 23606U 95033B 23272.76146346 .00009490 00000-0 73351-3 0 9994
2 23606 98.2694 18.9407 0009233 11.9779 348.1662 15.01722304529840
| Epoch (UTC): | 29 September 2023 18:16:30 |
| Eccentricity: | 0.0009233 |
| inclination: | 98.2694° |
| perigee height: | 555 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 18.9407° |
| argument of perigee: | 11.9779° |
| revolutions per day: | 15.01722304 |
| mean anomaly at epoch: | 348.1662° |
| orbit number at epoch: | 52984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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