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 65067U 26145.47713796 +.00000000 +00000-0 +37225-3 0 00001
2 65067 97.4499 222.5281 0002405 149.1589 210.9780 15.05656946 02
| Epoch (UTC): | 25 May 2026 11:27:04 |
| Eccentricity: | 0.0002405 |
| inclination: | 97.4499° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5281° |
| argument of perigee: | 149.1589° |
| revolutions per day: | 15.05656946 |
| mean anomaly at epoch: | 210.9780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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