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 56704U 26145.20108787 +.00000000 +00000-0 +63397-4 0 00008
2 56704 43.0024 198.7641 0001302 277.5897 82.4807 15.27577712 07
| Epoch (UTC): | 25 May 2026 04:49:33 |
| Eccentricity: | 0.0001302 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 198.7641° |
| argument of perigee: | 277.5897° |
| revolutions per day: | 15.27577712 |
| mean anomaly at epoch: | 82.4807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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