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 48641U 26145.12029208 +.00000000 +00000-0 -45175-5 0 00006
2 48641 53.1609 118.6051 0001287 83.5482 276.5666 15.31700426 06
| Epoch (UTC): | 25 May 2026 02:53:13 |
| Eccentricity: | 0.0001287 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 118.6051° |
| argument of perigee: | 83.5482° |
| revolutions per day: | 15.31700426 |
| mean anomaly at epoch: | 276.5666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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