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 55264U 26145.36654384 +.00000000 +00000-0 +00000-0 0 00002
2 55264 2.2905 81.9337 0000853 35.4087 240.8662 0.99151137 00
| Epoch (UTC): | 25 May 2026 08:47:49 |
| Eccentricity: | 0.0000853 |
| inclination: | 2.2905° |
| perigee height: | 36100 km |
| apogee height: | 36107 km |
| right ascension of ascending node: | 81.9337° |
| argument of perigee: | 35.4087° |
| revolutions per day: | 0.99151137 |
| mean anomaly at epoch: | 240.8662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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