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 65139U 26145.46692721 +.00000000 +00000-0 +28802-3 0 00005
2 65139 51.8996 171.0534 0000312 68.6403 291.4593 14.79941847 05
| Epoch (UTC): | 25 May 2026 11:12:22 |
| Eccentricity: | 0.0000312 |
| inclination: | 51.8996° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 171.0534° |
| argument of perigee: | 68.6403° |
| revolutions per day: | 14.79941847 |
| mean anomaly at epoch: | 291.4593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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