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 48594U 26145.19584007 +.00000000 +00000-0 -34874-5 0 00007
2 48594 53.1603 118.6313 0001043 89.4757 270.6363 15.29357911 01
| Epoch (UTC): | 25 May 2026 04:42:00 |
| Eccentricity: | 0.0001043 |
| inclination: | 53.1603° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 118.6313° |
| argument of perigee: | 89.4757° |
| revolutions per day: | 15.29357911 |
| mean anomaly at epoch: | 270.6363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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