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 59394U 26145.57410331 +.00000000 +00000-0 +14507-3 0 00005
2 59394 53.1627 258.4776 0001288 102.0414 258.0732 15.30174987 08
| Epoch (UTC): | 25 May 2026 13:46:42 |
| Eccentricity: | 0.0001288 |
| inclination: | 53.1627° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 258.4776° |
| argument of perigee: | 102.0414° |
| revolutions per day: | 15.30174987 |
| mean anomaly at epoch: | 258.0732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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