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 55469U 26145.58608256 +.00000000 +00000-0 +18954-4 0 00001
2 55469 43.0034 254.3344 0001286 274.4502 85.6203 15.27575570 09
| Epoch (UTC): | 25 May 2026 14:03:57 |
| Eccentricity: | 0.0001286 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.3344° |
| argument of perigee: | 274.4502° |
| revolutions per day: | 15.27575570 |
| mean anomaly at epoch: | 85.6203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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