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 48650U 26145.21348809 +.00000000 +00000-0 +99221-4 0 00006
2 48650 53.1570 118.0352 0001036 95.0006 265.1114 15.31706510 05
| Epoch (UTC): | 25 May 2026 05:07:25 |
| Eccentricity: | 0.0001036 |
| inclination: | 53.1570° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 118.0352° |
| argument of perigee: | 95.0006° |
| revolutions per day: | 15.31706510 |
| mean anomaly at epoch: | 265.1114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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