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 65152U 26145.51555133 +.00000000 +00000-0 +12704-2 0 00004
2 65152 51.8978 188.3642 0000070 138.6726 221.4242 14.79983089 06
| Epoch (UTC): | 25 May 2026 12:22:23 |
| Eccentricity: | 0.0000070 |
| inclination: | 51.8978° |
| perigee height: | 629 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 188.3642° |
| argument of perigee: | 138.6726° |
| revolutions per day: | 14.79983089 |
| mean anomaly at epoch: | 221.4242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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