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 23342U 94074A 25196.79155899 .00000732 00000-0 93140-4 0 9997
2 23342 97.6892 222.6356 0002181 96.0020 264.1444 14.84394014654011
| Epoch (UTC): | 15 July 2025 18:59:50 |
| Eccentricity: | 0.0002181 |
| inclination: | 97.6892° |
| perigee height: | 614 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 222.6356° |
| argument of perigee: | 96.0020° |
| revolutions per day: | 14.84394014 |
| mean anomaly at epoch: | 264.1444° |
| orbit number at epoch: | 65401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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