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 55993U 26145.53885426 +.00000000 +00000-0 -64683-5 0 00006
2 55993 43.0065 345.5139 0001719 263.7844 96.2812 15.27574087 07
| Epoch (UTC): | 25 May 2026 12:55:57 |
| Eccentricity: | 0.0001719 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.5139° |
| argument of perigee: | 263.7844° |
| revolutions per day: | 15.27574087 |
| mean anomaly at epoch: | 96.2812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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