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 55603U 26145.66495985 +.00000000 +00000-0 +46231-4 0 00002
2 55603 43.0007 279.3521 0001217 276.3443 83.7270 15.27577456 00
| Epoch (UTC): | 25 May 2026 15:57:32 |
| Eccentricity: | 0.0001217 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 279.3521° |
| argument of perigee: | 276.3443° |
| revolutions per day: | 15.27577456 |
| mean anomaly at epoch: | 83.7270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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