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 46048U 26145.30238916 +.00000000 +00000-0 +13430-3 0 00009
2 46048 53.1592 117.6722 0001524 78.3964 281.7209 15.31699020 09
| Epoch (UTC): | 25 May 2026 07:15:26 |
| Eccentricity: | 0.0001524 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.6722° |
| argument of perigee: | 78.3964° |
| revolutions per day: | 15.31699020 |
| mean anomaly at epoch: | 281.7209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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