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 65927U 26145.47892932 +.00000000 +00000-0 +69034-3 0 00009
2 65927 53.1591 169.0911 0001118 79.4511 280.6617 15.34394411 05
| Epoch (UTC): | 25 May 2026 11:29:39 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 169.0911° |
| argument of perigee: | 79.4511° |
| revolutions per day: | 15.34394411 |
| mean anomaly at epoch: | 280.6617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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