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 48596U 26145.28086625 +.00000000 +00000-0 +19228-4 0 00006
2 48596 53.1571 143.3153 0001207 80.5943 279.5195 15.31703349 09
| Epoch (UTC): | 25 May 2026 06:44:26 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1571° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 143.3153° |
| argument of perigee: | 80.5943° |
| revolutions per day: | 15.31703349 |
| mean anomaly at epoch: | 279.5195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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