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 48276U 26145.15138001 +.00000000 +00000-0 +10394-3 0 00007
2 48276 53.1611 55.3011 0001254 94.8239 265.2905 15.31713037 08
| Epoch (UTC): | 25 May 2026 03:37:59 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.3011° |
| argument of perigee: | 94.8239° |
| revolutions per day: | 15.31713037 |
| mean anomaly at epoch: | 265.2905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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