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 56289U 26145.36700488 +.00000000 +00000-0 +81991-4 0 00009
2 56289 43.0024 109.9997 0001128 255.0603 105.0124 15.27584582 02
| Epoch (UTC): | 25 May 2026 08:48:29 |
| Eccentricity: | 0.0001128 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 109.9997° |
| argument of perigee: | 255.0603° |
| revolutions per day: | 15.27584582 |
| mean anomaly at epoch: | 105.0124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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