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 67517U 26145.59178281 +.00000000 +00000-0 +44534-3 0 00001
2 67517 43.0034 240.0387 0001560 265.3343 94.7331 15.27594163 04
| Epoch (UTC): | 25 May 2026 14:12:10 |
| Eccentricity: | 0.0001560 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.0387° |
| argument of perigee: | 265.3343° |
| revolutions per day: | 15.27594163 |
| mean anomaly at epoch: | 94.7331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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