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 48142U 26145.41419948 +.00000000 +00000-0 +12413-3 0 00004
2 48142 53.1590 156.1969 0001225 89.1933 270.9208 15.31712201 05
| Epoch (UTC): | 25 May 2026 09:56:26 |
| Eccentricity: | 0.0001225 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 156.1969° |
| argument of perigee: | 89.1933° |
| revolutions per day: | 15.31712201 |
| mean anomaly at epoch: | 270.9208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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