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 56421U 26145.50003470 +.00000000 +00000-0 +89771-4 0 00004
2 56421 43.0006 109.3421 0001711 282.2822 125.3944 15.27582311 02
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001711 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 109.3421° |
| argument of perigee: | 282.2822° |
| revolutions per day: | 15.27582311 |
| mean anomaly at epoch: | 125.3944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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