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 59466U 26145.51901090 +.00000000 +00000-0 +25037-4 0 00007
2 59466 43.0041 320.5340 0001464 273.0150 87.0534 15.27574878 05
| Epoch (UTC): | 25 May 2026 12:27:22 |
| Eccentricity: | 0.0001464 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.5340° |
| argument of perigee: | 273.0150° |
| revolutions per day: | 15.27574878 |
| mean anomaly at epoch: | 87.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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