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 54852U 26144.79137176 +.00000000 +00000-0 +10008-3 0 00007
2 54852 43.0067 51.4360 0001263 262.7926 97.2782 15.27583012 00
| Epoch (UTC): | 24 May 2026 18:59:34 |
| Eccentricity: | 0.0001263 |
| inclination: | 43.0067° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 51.4360° |
| argument of perigee: | 262.7926° |
| revolutions per day: | 15.27583012 |
| mean anomaly at epoch: | 97.2782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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