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 67443U 26145.33470750 +.00000000 +00000-0 +97187-4 0 00000
2 67443 50.0072 167.4592 0000842 281.4009 78.6768 13.29324661 01
| Epoch (UTC): | 25 May 2026 08:01:58 |
| Eccentricity: | 0.0000842 |
| inclination: | 50.0072° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.4592° |
| argument of perigee: | 281.4009° |
| revolutions per day: | 13.29324661 |
| mean anomaly at epoch: | 78.6768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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