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 65922U 26145.34623265 +.00000000 +00000-0 +61473-3 0 00000
2 65922 53.1594 169.6862 0000912 87.0355 273.0752 15.33562319 05
| Epoch (UTC): | 25 May 2026 08:18:34 |
| Eccentricity: | 0.0000912 |
| inclination: | 53.1594° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 169.6862° |
| argument of perigee: | 87.0355° |
| revolutions per day: | 15.33562319 |
| mean anomaly at epoch: | 273.0752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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