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 48432U 26145.41883844 +.00000000 +00000-0 -18540-3 0 00004
2 48432 53.1598 156.0355 0001321 82.9186 277.1966 15.31677722 09
| Epoch (UTC): | 25 May 2026 10:03:07 |
| Eccentricity: | 0.0001321 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 156.0355° |
| argument of perigee: | 82.9186° |
| revolutions per day: | 15.31677722 |
| mean anomaly at epoch: | 277.1966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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