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 55589U 26145.45978359 +.00000000 +00000-0 -26744-4 0 00001
2 55589 43.0033 291.6560 0001283 270.3947 89.6758 15.27574895 08
| Epoch (UTC): | 25 May 2026 11:02:05 |
| Eccentricity: | 0.0001283 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.6560° |
| argument of perigee: | 270.3947° |
| revolutions per day: | 15.27574895 |
| mean anomaly at epoch: | 89.6758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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