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 48096U 26145.30602718 +.00000000 +00000-0 -18349-2 0 00003
2 48096 53.1587 169.2668 0001106 344.2842 15.8125 15.31278208 00
| Epoch (UTC): | 25 May 2026 07:20:40 |
| Eccentricity: | 0.0001106 |
| inclination: | 53.1587° |
| perigee height: | 471 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 169.2668° |
| argument of perigee: | 344.2842° |
| revolutions per day: | 15.31278208 |
| mean anomaly at epoch: | 15.8125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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