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 64850U 26145.09754362 +.00000000 +00000-0 +26542-3 0 00002
2 64850 97.4520 0.4270 0001655 81.6474 278.4941 15.05658874 06
| Epoch (UTC): | 25 May 2026 02:20:27 |
| Eccentricity: | 0.0001655 |
| inclination: | 97.4520° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.4270° |
| argument of perigee: | 81.6474° |
| revolutions per day: | 15.05658874 |
| mean anomaly at epoch: | 278.4941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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