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 64188U 26145.29875741 +.00000000 +00000-0 +51162-3 0 00009
2 64188 53.1575 95.3338 0002094 20.2812 339.8272 15.30219074 02
| Epoch (UTC): | 25 May 2026 07:10:12 |
| Eccentricity: | 0.0002094 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 95.3338° |
| argument of perigee: | 20.2812° |
| revolutions per day: | 15.30219074 |
| mean anomaly at epoch: | 339.8272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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