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 48045U 26145.23439734 +.00000000 +00000-0 -51047-3 0 00008
2 48045 87.8941 324.7933 0001727 89.7375 270.3952 13.13469110 04
| Epoch (UTC): | 25 May 2026 05:37:31 |
| Eccentricity: | 0.0001727 |
| inclination: | 87.8941° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7933° |
| argument of perigee: | 89.7375° |
| revolutions per day: | 13.13469110 |
| mean anomaly at epoch: | 270.3952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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