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 67437U 26145.46000682 +.00000000 +00000-0 +36786-4 0 00008
2 67437 50.0004 167.3720 0000898 276.2802 83.7967 13.29307746 08
| Epoch (UTC): | 25 May 2026 11:02:24 |
| Eccentricity: | 0.0000898 |
| inclination: | 50.0004° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.3720° |
| argument of perigee: | 276.2802° |
| revolutions per day: | 13.29307746 |
| mean anomaly at epoch: | 83.7967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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