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 67240U 26145.52432878 +.00000000 +00000-0 +67074-4 0 00007
2 67240 50.0045 197.1543 0001014 246.6843 113.3922 13.29323129 00
| Epoch (UTC): | 25 May 2026 12:35:02 |
| Eccentricity: | 0.0001014 |
| inclination: | 50.0045° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 197.1543° |
| argument of perigee: | 246.6843° |
| revolutions per day: | 13.29323129 |
| mean anomaly at epoch: | 113.3922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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