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 is defined by the following mean orbital elements,
1 34839U 09021A 25168.22293757 .17838157 25147-5 10000-3 0 9996
2 34839 97.1678 151.1992 0011592 251.8613 231.0861 16.54800084900690
| Epoch (UTC): | 17 June 2025 05:21:01 |
| Eccentricity: | 0.0011592 |
| inclination: | 97.1678° |
| perigee height: | 119 km |
| apogee height: | 134 km |
| right ascension of ascending node: | 151.1992° |
| argument of perigee: | 251.8613° |
| revolutions per day: | 16.54800084 |
| mean anomaly at epoch: | 231.0861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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