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 67238U 26145.39067650 +.00000000 +00000-0 +58724-4 0 00003
2 67238 50.0036 197.7694 0001041 247.8368 112.2394 13.29322623 04
| Epoch (UTC): | 25 May 2026 09:22:34 |
| Eccentricity: | 0.0001041 |
| inclination: | 50.0036° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.7694° |
| argument of perigee: | 247.8368° |
| revolutions per day: | 13.29322623 |
| mean anomaly at epoch: | 112.2394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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