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 48646U 26145.21814215 +.00000000 +00000-0 +81071-5 0 00005
2 48646 53.1577 117.9480 0001238 95.9256 264.1887 15.31701722 03
| Epoch (UTC): | 25 May 2026 05:14:07 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.9480° |
| argument of perigee: | 95.9256° |
| revolutions per day: | 15.31701722 |
| mean anomaly at epoch: | 264.1887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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