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 65355U 26145.48119037 +.00000000 +00000-0 +35384-3 0 00004
2 65355 53.1583 171.3983 0000950 78.8215 281.2893 15.30204917 03
| Epoch (UTC): | 25 May 2026 11:32:54 |
| Eccentricity: | 0.0000950 |
| inclination: | 53.1583° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.3983° |
| argument of perigee: | 78.8215° |
| revolutions per day: | 15.30204917 |
| mean anomaly at epoch: | 281.2893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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