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 67765U 26145.56072795 +.00000000 +00000-0 +78729-3 0 00009
2 67765 51.8800 207.8359 0006517 333.6784 26.3871 15.37937596 04
| Epoch (UTC): | 25 May 2026 13:27:26 |
| Eccentricity: | 0.0006517 |
| inclination: | 51.8800° |
| perigee height: | 448 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 207.8359° |
| argument of perigee: | 333.6784° |
| revolutions per day: | 15.37937596 |
| mean anomaly at epoch: | 26.3871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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