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 64862U 26145.34123014 +.00000000 +00000-0 +74420-4 0 00006
2 64862 97.4482 0.7221 0001646 87.3551 272.7864 15.05653405 00
| Epoch (UTC): | 25 May 2026 08:11:22 |
| Eccentricity: | 0.0001646 |
| inclination: | 97.4482° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7221° |
| argument of perigee: | 87.3551° |
| revolutions per day: | 15.05653405 |
| mean anomaly at epoch: | 272.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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