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 48136U 26145.47346742 +.00000000 +00000-0 +38849-4 0 00006
2 48136 53.1589 168.4157 0001200 80.4430 279.6707 15.31701767 05
| Epoch (UTC): | 25 May 2026 11:21:47 |
| Eccentricity: | 0.0001200 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 168.4157° |
| argument of perigee: | 80.4430° |
| revolutions per day: | 15.31701767 |
| mean anomaly at epoch: | 279.6707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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