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 65918U 26145.32891950 +.00000000 +00000-0 +41351-3 0 00004
2 65918 53.1597 169.5729 0001176 83.3842 276.7292 15.30184002 02
| Epoch (UTC): | 25 May 2026 07:53:38 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.5729° |
| argument of perigee: | 83.3842° |
| revolutions per day: | 15.30184002 |
| mean anomaly at epoch: | 276.7292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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