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 67009U 26145.36042545 +.00000000 +00000-0 +28707-3 0 00009
2 67009 70.0005 261.0876 0003344 267.9037 92.1739 14.98339909 00
| Epoch (UTC): | 25 May 2026 08:39:00 |
| Eccentricity: | 0.0003344 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.0876° |
| argument of perigee: | 267.9037° |
| revolutions per day: | 14.98339909 |
| mean anomaly at epoch: | 92.1739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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