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 56420U 26145.27900649 +.00000000 +00000-0 +11185-2 0 00003
2 56420 43.0089 106.9698 0002605 265.3392 94.7162 15.27388428 02
| Epoch (UTC): | 25 May 2026 06:41:46 |
| Eccentricity: | 0.0002605 |
| inclination: | 43.0089° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 106.9698° |
| argument of perigee: | 265.3392° |
| revolutions per day: | 15.27388428 |
| mean anomaly at epoch: | 94.7162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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