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 56340U 26145.17408296 +.00000000 +00000-0 -70758-3 0 00007
2 56340 97.4468 146.2124 0001632 71.0223 289.1181 15.05698730 09
| Epoch (UTC): | 25 May 2026 04:10:40 |
| Eccentricity: | 0.0001632 |
| inclination: | 97.4468° |
| perigee height: | 548 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 146.2124° |
| argument of perigee: | 71.0223° |
| revolutions per day: | 15.05698730 |
| mean anomaly at epoch: | 289.1181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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