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 59639U 26145.48666873 +.00000000 +00000-0 +21397-4 0 00007
2 59639 43.0033 66.3942 0000911 274.5563 85.5185 15.27574083 04
| Epoch (UTC): | 25 May 2026 11:40:48 |
| Eccentricity: | 0.0000911 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.3942° |
| argument of perigee: | 274.5563° |
| revolutions per day: | 15.27574083 |
| mean anomaly at epoch: | 85.5185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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