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 67526U 26145.48826317 +.00000000 +00000-0 +77049-4 0 00007
2 67526 50.0049 76.8940 0000932 27.7181 332.3740 13.29327472 02
| Epoch (UTC): | 25 May 2026 11:43:05 |
| Eccentricity: | 0.0000932 |
| inclination: | 50.0049° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 76.8940° |
| argument of perigee: | 27.7181° |
| revolutions per day: | 13.29327472 |
| mean anomaly at epoch: | 332.3740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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