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 56064U 26145.50949691 +.00000000 +00000-0 +10856-3 0 00008
2 56064 87.9104 233.2703 0002469 98.7989 261.3422 13.16593245 02
| Epoch (UTC): | 25 May 2026 12:13:40 |
| Eccentricity: | 0.0002469 |
| inclination: | 87.9104° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2703° |
| argument of perigee: | 98.7989° |
| revolutions per day: | 13.16593245 |
| mean anomaly at epoch: | 261.3422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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