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 01778U 26152.46932896 +.00000000 +00000-0 +19985-3 0 00004
2 01778 34.2556 310.6187 0738809 88.3000 280.2055 13.49794387 07
| Epoch (UTC): | 01 June 2026 11:15:50 |
| Eccentricity: | 0.0738809 |
| inclination: | 34.2556° |
| perigee height: | 523 km |
| apogee height: | 1624 km |
| right ascension of ascending node: | 310.6187° |
| argument of perigee: | 88.3000° |
| revolutions per day: | 13.49794387 |
| mean anomaly at epoch: | 280.2055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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