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 45384U 26145.33902169 +.00000000 +00000-0 +84423-3 0 00002
2 45384 53.0435 115.4483 0007557 60.2930 299.8835 15.63289187 00
| Epoch (UTC): | 25 May 2026 08:08:11 |
| Eccentricity: | 0.0007557 |
| inclination: | 53.0435° |
| perigee height: | 373 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 115.4483° |
| argument of perigee: | 60.2930° |
| revolutions per day: | 15.63289187 |
| mean anomaly at epoch: | 299.8835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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