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 48558U 26145.25384845 +.00000000 +00000-0 +11892-4 0 00005
2 48558 53.1605 130.7415 0001121 93.2342 266.8788 15.31701217 04
| Epoch (UTC): | 25 May 2026 06:05:32 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.7415° |
| argument of perigee: | 93.2342° |
| revolutions per day: | 15.31701217 |
| mean anomaly at epoch: | 266.8788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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