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 65839U 26145.55566801 +.00000000 +00000-0 +83508-2 0 00004
2 65839 53.1593 91.1869 0001432 78.6851 281.4312 15.34245259 09
| Epoch (UTC): | 25 May 2026 13:20:09 |
| Eccentricity: | 0.0001432 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 91.1869° |
| argument of perigee: | 78.6851° |
| revolutions per day: | 15.34245259 |
| mean anomaly at epoch: | 281.4312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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