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 54822U 26145.46399942 +.00000000 +00000-0 +11467-4 0 00001
2 54822 43.0032 62.5947 0000984 263.0880 96.9860 15.27576639 05
| Epoch (UTC): | 25 May 2026 11:08:09 |
| Eccentricity: | 0.0000984 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.5947° |
| argument of perigee: | 263.0880° |
| revolutions per day: | 15.27576639 |
| mean anomaly at epoch: | 96.9860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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