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 48144U 26145.43275466 +.00000000 +00000-0 +47204-4 0 00000
2 48144 53.1595 155.5640 0001182 90.2397 269.8740 15.31709301 05
| Epoch (UTC): | 25 May 2026 10:23:10 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.5640° |
| argument of perigee: | 90.2397° |
| revolutions per day: | 15.31709301 |
| mean anomaly at epoch: | 269.8740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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