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 48433U 26145.43744144 +.00000000 +00000-0 +43610-4 0 00002
2 48433 53.1580 155.6564 0001303 83.2177 276.8972 15.31710406 02
| Epoch (UTC): | 25 May 2026 10:29:54 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.6564° |
| argument of perigee: | 83.2177° |
| revolutions per day: | 15.31710406 |
| mean anomaly at epoch: | 276.8972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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