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 55324U 26145.36093767 +.00000000 +00000-0 +18691-3 0 00009
2 55324 40.4980 125.1871 0004543 245.0902 114.9435 15.22698031 03
| Epoch (UTC): | 25 May 2026 08:39:45 |
| Eccentricity: | 0.0004543 |
| inclination: | 40.4980° |
| perigee height: | 495 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 125.1871° |
| argument of perigee: | 245.0902° |
| revolutions per day: | 15.22698031 |
| mean anomaly at epoch: | 114.9435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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