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 56767U 26145.37675510 +.00000000 +00000-0 +11383-2 0 00004
2 56767 69.9883 150.1813 0003257 353.5595 6.5532 15.19662497 08
| Epoch (UTC): | 25 May 2026 09:02:31 |
| Eccentricity: | 0.0003257 |
| inclination: | 69.9883° |
| perigee height: | 505 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 150.1813° |
| argument of perigee: | 353.5595° |
| revolutions per day: | 15.19662497 |
| mean anomaly at epoch: | 6.5532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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