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 48323U 26145.28498466 +.00000000 +00000-0 +53960-4 0 00005
2 48323 53.1595 104.7947 0001240 81.7034 278.4108 15.31705342 03
| Epoch (UTC): | 25 May 2026 06:50:22 |
| Eccentricity: | 0.0001240 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.7947° |
| argument of perigee: | 81.7034° |
| revolutions per day: | 15.31705342 |
| mean anomaly at epoch: | 278.4108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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