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 64852U 26145.35783937 +.00000000 +00000-0 +19203-3 0 00009
2 64852 97.4478 0.6927 0002067 76.7121 283.4337 15.05658516 01
| Epoch (UTC): | 25 May 2026 08:35:17 |
| Eccentricity: | 0.0002067 |
| inclination: | 97.4478° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.6927° |
| argument of perigee: | 76.7121° |
| revolutions per day: | 15.05658516 |
| mean anomaly at epoch: | 283.4337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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