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 48659U 26145.10628742 +.00000000 +00000-0 +45140-4 0 00001
2 48659 53.1597 118.4392 0001379 81.7950 278.3208 15.31694371 02
| Epoch (UTC): | 25 May 2026 02:33:03 |
| Eccentricity: | 0.0001379 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 118.4392° |
| argument of perigee: | 81.7950° |
| revolutions per day: | 15.31694371 |
| mean anomaly at epoch: | 278.3208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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