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 67502U 26145.58792575 +.00000000 +00000-0 +64332-3 0 00000
2 67502 43.0017 240.0144 0002899 261.6750 98.3773 15.27596093 01
| Epoch (UTC): | 25 May 2026 14:06:36 |
| Eccentricity: | 0.0002899 |
| inclination: | 43.0017° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 240.0144° |
| argument of perigee: | 261.6750° |
| revolutions per day: | 15.27596093 |
| mean anomaly at epoch: | 98.3773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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