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 48651U 26145.20882885 +.00000000 +00000-0 +47929-4 0 00001
2 48651 53.1602 118.0502 0001130 79.4241 280.6887 15.31700985 00
| Epoch (UTC): | 25 May 2026 05:00:42 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 118.0502° |
| argument of perigee: | 79.4241° |
| revolutions per day: | 15.31700985 |
| mean anomaly at epoch: | 280.6887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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