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 56295U 26145.61584622 +.00000000 +00000-0 +22385-4 0 00006
2 56295 43.0044 109.2693 0001101 272.7287 87.3438 15.27577088 05
| Epoch (UTC): | 25 May 2026 14:46:49 |
| Eccentricity: | 0.0001101 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 109.2693° |
| argument of perigee: | 272.7287° |
| revolutions per day: | 15.27577088 |
| mean anomaly at epoch: | 87.3438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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