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 67521U 26145.58150690 +.00000000 +00000-0 +61290-3 0 00007
2 67521 43.0034 239.9624 0000304 289.7701 70.3118 15.27599549 09
| Epoch (UTC): | 25 May 2026 13:57:22 |
| Eccentricity: | 0.0000304 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 239.9624° |
| argument of perigee: | 289.7701° |
| revolutions per day: | 15.27599549 |
| mean anomaly at epoch: | 70.3118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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