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 67206U 26145.54929866 +.00000000 +00000-0 +17325-3 0 00002
2 67206 70.0017 340.8192 0002750 266.4514 93.6331 14.98334039 06
| Epoch (UTC): | 25 May 2026 13:10:59 |
| Eccentricity: | 0.0002750 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.8192° |
| argument of perigee: | 266.4514° |
| revolutions per day: | 14.98334039 |
| mean anomaly at epoch: | 93.6331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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