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 48148U 26145.44085951 +.00000000 +00000-0 -12702-4 0 00009
2 48148 53.1598 168.7413 0001158 87.5843 272.5291 15.31700152 01
| Epoch (UTC): | 25 May 2026 10:34:50 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 168.7413° |
| argument of perigee: | 87.5843° |
| revolutions per day: | 15.31700152 |
| mean anomaly at epoch: | 272.5291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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