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 67439U 26145.44327799 +.00000000 +00000-0 +84725-4 0 00005
2 67439 50.0022 167.3051 0000883 283.0539 77.0234 13.29325730 00
| Epoch (UTC): | 25 May 2026 10:38:19 |
| Eccentricity: | 0.0000883 |
| inclination: | 50.0022° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 167.3051° |
| argument of perigee: | 283.0539° |
| revolutions per day: | 13.29325730 |
| mean anomaly at epoch: | 77.0234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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