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 48649U 26145.33465199 +.00000000 +00000-0 +29972-4 0 00005
2 48649 53.1597 117.3384 0001180 87.2555 272.8581 15.31705148 00
| Epoch (UTC): | 25 May 2026 08:01:53 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.3384° |
| argument of perigee: | 87.2555° |
| revolutions per day: | 15.31705148 |
| mean anomaly at epoch: | 272.8581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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