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 64816U 26145.42801722 +.00000000 +00000-0 +49140-3 0 00003
2 64816 51.9018 301.2988 0000604 112.1562 247.9465 14.79936824 00
| Epoch (UTC): | 25 May 2026 10:16:20 |
| Eccentricity: | 0.0000604 |
| inclination: | 51.9018° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 301.2988° |
| argument of perigee: | 112.1562° |
| revolutions per day: | 14.79936824 |
| mean anomaly at epoch: | 247.9465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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