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 48652U 26145.33691565 +.00000000 +00000-0 +75271-3 0 00009
2 48652 53.0485 103.8418 0001327 126.4287 233.6853 15.70576338 05
| Epoch (UTC): | 25 May 2026 08:05:09 |
| Eccentricity: | 0.0001327 |
| inclination: | 53.0485° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 103.8418° |
| argument of perigee: | 126.4287° |
| revolutions per day: | 15.70576338 |
| mean anomaly at epoch: | 233.6853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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