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 64244U 26145.37921676 +.00000000 +00000-0 +12639-2 0 00005
2 64244 42.9996 107.0626 0001206 261.2584 98.8147 15.70877607 05
| Epoch (UTC): | 25 May 2026 09:06:04 |
| Eccentricity: | 0.0001206 |
| inclination: | 42.9996° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 107.0626° |
| argument of perigee: | 261.2584° |
| revolutions per day: | 15.70877607 |
| mean anomaly at epoch: | 98.8147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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