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 59413U 26145.57497267 +.00000000 +00000-0 -11670-3 0 00009
2 59413 43.0039 335.0895 0000878 274.1400 85.9352 15.27555834 04
| Epoch (UTC): | 25 May 2026 13:47:57 |
| Eccentricity: | 0.0000878 |
| inclination: | 43.0039° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.0895° |
| argument of perigee: | 274.1400° |
| revolutions per day: | 15.27555834 |
| mean anomaly at epoch: | 85.9352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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