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 48555U 26145.29678086 +.00000000 +00000-0 +27685-4 0 00006
2 48555 53.1588 152.6386 0001164 77.6055 282.5077 15.31702216 01
| Epoch (UTC): | 25 May 2026 07:07:21 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 152.6386° |
| argument of perigee: | 77.6055° |
| revolutions per day: | 15.31702216 |
| mean anomaly at epoch: | 282.5077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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