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 64946U 26145.35843681 +.00000000 +00000-0 +22560-3 0 00006
2 64946 97.4514 9.2919 0002465 87.2176 272.9333 15.05656845 03
| Epoch (UTC): | 25 May 2026 08:36:08 |
| Eccentricity: | 0.0002465 |
| inclination: | 97.4514° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.2919° |
| argument of perigee: | 87.2176° |
| revolutions per day: | 15.05656845 |
| mean anomaly at epoch: | 272.9333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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