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 54056U 26145.28769958 +.00000000 +00000-0 +76317-5 0 00004
2 54056 53.2116 359.8443 0001270 82.0196 278.0941 15.08834316 02
| Epoch (UTC): | 25 May 2026 06:54:17 |
| Eccentricity: | 0.0001270 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 359.8443° |
| argument of perigee: | 82.0196° |
| revolutions per day: | 15.08834316 |
| mean anomaly at epoch: | 278.0941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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