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 48134U 26145.35693431 +.00000000 +00000-0 -31554-3 0 00007
2 48134 53.1568 168.6627 0001367 81.9185 278.1971 15.31657132 04
| Epoch (UTC): | 25 May 2026 08:33:59 |
| Eccentricity: | 0.0001367 |
| inclination: | 53.1568° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 168.6627° |
| argument of perigee: | 81.9185° |
| revolutions per day: | 15.31657132 |
| mean anomaly at epoch: | 278.1971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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