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 67062U 26145.35211359 +.00000000 +00000-0 +86490-4 0 00002
2 67062 50.0025 107.4603 0000833 354.1997 5.8866 13.29328770 03
| Epoch (UTC): | 25 May 2026 08:27:02 |
| Eccentricity: | 0.0000833 |
| inclination: | 50.0025° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 107.4603° |
| argument of perigee: | 354.1997° |
| revolutions per day: | 13.29328770 |
| mean anomaly at epoch: | 5.8866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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