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 65350U 26145.56724906 +.00000000 +00000-0 +89565-3 0 00005
2 65350 53.1599 209.1879 0000844 64.6429 295.4659 15.31716195 05
| Epoch (UTC): | 25 May 2026 13:36:50 |
| Eccentricity: | 0.0000844 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.1879° |
| argument of perigee: | 64.6429° |
| revolutions per day: | 15.31716195 |
| mean anomaly at epoch: | 295.4659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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