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 56008U 26145.60037972 +.00000000 +00000-0 -45732-5 0 00001
2 56008 43.0064 345.0955 0001463 262.6403 97.4282 15.27575668 00
| Epoch (UTC): | 25 May 2026 14:24:32 |
| Eccentricity: | 0.0001463 |
| inclination: | 43.0064° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.0955° |
| argument of perigee: | 262.6403° |
| revolutions per day: | 15.27575668 |
| mean anomaly at epoch: | 97.4282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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