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 59439U 26145.37403676 +.00000000 +00000-0 +25164-4 0 00009
2 59439 53.1609 285.2288 0001106 103.3869 256.7255 15.30190013 04
| Epoch (UTC): | 25 May 2026 08:58:36 |
| Eccentricity: | 0.0001106 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 285.2288° |
| argument of perigee: | 103.3869° |
| revolutions per day: | 15.30190013 |
| mean anomaly at epoch: | 256.7255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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