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 59340U 26145.37257384 +.00000000 +00000-0 +19146-4 0 00006
2 59340 43.0009 128.9921 0001022 270.3343 89.7391 15.27575546 02
| Epoch (UTC): | 25 May 2026 08:56:30 |
| Eccentricity: | 0.0001022 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.9921° |
| argument of perigee: | 270.3343° |
| revolutions per day: | 15.27575546 |
| mean anomaly at epoch: | 89.7391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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