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 56342U 26145.28208860 +.00000000 +00000-0 -43524-4 0 00008
2 56342 97.4468 146.3735 0003426 102.7011 257.4599 15.05656325 05
| Epoch (UTC): | 25 May 2026 06:46:12 |
| Eccentricity: | 0.0003426 |
| inclination: | 97.4468° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 146.3735° |
| argument of perigee: | 102.7011° |
| revolutions per day: | 15.05656325 |
| mean anomaly at epoch: | 257.4599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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