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 48326U 26145.28067203 +.00000000 +00000-0 +54714-3 0 00006
2 48326 53.1600 104.8755 0001471 84.5552 275.5618 15.31710690 09
| Epoch (UTC): | 25 May 2026 06:44:10 |
| Eccentricity: | 0.0001471 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.8755° |
| argument of perigee: | 84.5552° |
| revolutions per day: | 15.31710690 |
| mean anomaly at epoch: | 275.5618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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