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 64391U 26145.34310912 +.00000000 +00000-0 +61365-3 0 00001
2 64391 43.0008 106.5842 0001959 253.3673 106.6963 15.27589103 01
| Epoch (UTC): | 25 May 2026 08:14:04 |
| Eccentricity: | 0.0001959 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.5842° |
| argument of perigee: | 253.3673° |
| revolutions per day: | 15.27589103 |
| mean anomaly at epoch: | 106.6963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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