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 64947U 26145.10367488 +.00000000 +00000-0 +30678-3 0 00005
2 64947 97.4518 9.0268 0001561 122.3599 237.7780 15.05661822 05
| Epoch (UTC): | 25 May 2026 02:29:17 |
| Eccentricity: | 0.0001561 |
| inclination: | 97.4518° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.0268° |
| argument of perigee: | 122.3599° |
| revolutions per day: | 15.05661822 |
| mean anomaly at epoch: | 237.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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