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 48578U 26145.44026310 +.00000000 +00000-0 +11511-3 0 00005
2 48578 53.1573 129.7707 0001254 90.4922 269.6224 15.31705519 07
| Epoch (UTC): | 25 May 2026 10:33:58 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1573° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 129.7707° |
| argument of perigee: | 90.4922° |
| revolutions per day: | 15.31705519 |
| mean anomaly at epoch: | 269.6224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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