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 48639U 26145.39558250 +.00000000 +00000-0 +12726-3 0 00009
2 48639 53.1579 117.0809 0001177 85.6371 274.4765 15.31699786 04
| Epoch (UTC): | 25 May 2026 09:29:38 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.0809° |
| argument of perigee: | 85.6371° |
| revolutions per day: | 15.31699786 |
| mean anomaly at epoch: | 274.4765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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