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 59663U 26145.22958911 +.00000000 +00000-0 +37377-4 0 00008
2 59663 43.0036 329.1792 0001414 276.9302 83.1388 15.27576621 02
| Epoch (UTC): | 25 May 2026 05:30:36 |
| Eccentricity: | 0.0001414 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 329.1792° |
| argument of perigee: | 276.9302° |
| revolutions per day: | 15.27576621 |
| mean anomaly at epoch: | 83.1388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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