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 48064U 26145.49933781 +.00000000 +00000-0 +42401-3 0 00001
2 48064 87.8941 324.7510 0001109 94.0849 266.0407 13.13470608 06
| Epoch (UTC): | 25 May 2026 11:59:02 |
| Eccentricity: | 0.0001109 |
| inclination: | 87.8941° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7510° |
| argument of perigee: | 94.0849° |
| revolutions per day: | 13.13470608 |
| mean anomaly at epoch: | 266.0407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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