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 48964U 26145.50220164 +.00000000 +00000-0 +42375-3 0 00006
2 48964 97.6795 343.5735 0001732 76.8088 283.3370 15.76123132 03
| Epoch (UTC): | 25 May 2026 12:03:10 |
| Eccentricity: | 0.0001732 |
| inclination: | 97.6795° |
| perigee height: | 340 km |
| apogee height: | 343 km |
| right ascension of ascending node: | 343.5735° |
| argument of perigee: | 76.8088° |
| revolutions per day: | 15.76123132 |
| mean anomaly at epoch: | 283.3370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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