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 59339U 26145.40762144 +.00000000 +00000-0 +89794-4 0 00009
2 59339 43.0019 113.6746 0000605 281.9906 78.0878 15.27577666 02
| Epoch (UTC): | 25 May 2026 09:46:58 |
| Eccentricity: | 0.0000605 |
| inclination: | 43.0019° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 113.6746° |
| argument of perigee: | 281.9906° |
| revolutions per day: | 15.27577666 |
| mean anomaly at epoch: | 78.0878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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