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 48425U 26145.52903727 +.00000000 +00000-0 +13798-3 0 00000
2 48425 34.9937 168.8246 0002880 248.1311 111.9091 15.02475496 08
| Epoch (UTC): | 25 May 2026 12:41:48 |
| Eccentricity: | 0.0002880 |
| inclination: | 34.9937° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 168.8246° |
| argument of perigee: | 248.1311° |
| revolutions per day: | 15.02475496 |
| mean anomaly at epoch: | 111.9091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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