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 64518U 26145.55485691 +.00000000 +00000-0 +17674-3 0 00006
2 64518 51.9003 245.6361 0001011 118.5515 241.5549 14.79935822 00
| Epoch (UTC): | 25 May 2026 13:18:59 |
| Eccentricity: | 0.0001011 |
| inclination: | 51.9003° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 245.6361° |
| argument of perigee: | 118.5515° |
| revolutions per day: | 14.79935822 |
| mean anomaly at epoch: | 241.5549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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