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 48113U 26145.34758896 +.00000000 +00000-0 +44152-4 0 00008
2 48113 53.1587 168.7593 0001094 86.5291 273.5836 15.31706838 08
| Epoch (UTC): | 25 May 2026 08:20:31 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 168.7593° |
| argument of perigee: | 86.5291° |
| revolutions per day: | 15.31706838 |
| mean anomaly at epoch: | 273.5836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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