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 48112U 26145.33796316 +.00000000 +00000-0 +17583-1 0 00000
2 48112 53.1580 171.2773 0010007 149.8779 210.2801 15.33488578 07
| Epoch (UTC): | 25 May 2026 08:06:40 |
| Eccentricity: | 0.0010007 |
| inclination: | 53.1580° |
| perigee height: | 459 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 171.2773° |
| argument of perigee: | 149.8779° |
| revolutions per day: | 15.33488578 |
| mean anomaly at epoch: | 210.2801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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