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 67528U 26145.47988875 +.00000000 +00000-0 +88517-4 0 00008
2 67528 50.0043 76.8433 0000924 27.9858 332.1064 13.29327967 05
| Epoch (UTC): | 25 May 2026 11:31:02 |
| Eccentricity: | 0.0000924 |
| inclination: | 50.0043° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 76.8433° |
| argument of perigee: | 27.9858° |
| revolutions per day: | 13.29327967 |
| mean anomaly at epoch: | 332.1064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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