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 48135U 26145.37159006 +.00000000 +00000-0 +54191-4 0 00007
2 48135 53.1568 171.3072 0001007 93.2404 266.8713 15.31704487 05
| Epoch (UTC): | 25 May 2026 08:55:05 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1568° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 171.3072° |
| argument of perigee: | 93.2404° |
| revolutions per day: | 15.31704487 |
| mean anomaly at epoch: | 266.8713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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