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 64944U 26145.05382785 +.00000000 +00000-0 +29582-3 0 00005
2 64944 97.4522 8.9377 0002041 101.9935 258.1521 15.05669225 02
| Epoch (UTC): | 25 May 2026 01:17:30 |
| Eccentricity: | 0.0002041 |
| inclination: | 97.4522° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.9377° |
| argument of perigee: | 101.9935° |
| revolutions per day: | 15.05669225 |
| mean anomaly at epoch: | 258.1521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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