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 55497U 26145.38862071 +.00000000 +00000-0 +19282-4 0 00002
2 55497 43.0048 266.7155 0001992 282.1638 77.8990 15.27576226 07
| Epoch (UTC): | 25 May 2026 09:19:36 |
| Eccentricity: | 0.0001992 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.7155° |
| argument of perigee: | 282.1638° |
| revolutions per day: | 15.27576226 |
| mean anomaly at epoch: | 77.8990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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