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 55602U 26145.43553537 +.00000000 +00000-0 +10385-4 0 00005
2 55602 43.0022 281.0494 0001741 276.1985 83.8668 15.27576830 03
| Epoch (UTC): | 25 May 2026 10:27:10 |
| Eccentricity: | 0.0001741 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 281.0494° |
| argument of perigee: | 276.1985° |
| revolutions per day: | 15.27576830 |
| mean anomaly at epoch: | 83.8668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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