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 67557U 26145.64454716 +.00000000 +00000-0 +51968-4 0 00001
2 67557 88.9986 270.8216 0004887 126.0049 234.1557 13.52666634 04
| Epoch (UTC): | 25 May 2026 15:28:08 |
| Eccentricity: | 0.0004887 |
| inclination: | 88.9986° |
| perigee height: | 1059 km |
| apogee height: | 1066 km |
| right ascension of ascending node: | 270.8216° |
| argument of perigee: | 126.0049° |
| revolutions per day: | 13.52666634 |
| mean anomaly at epoch: | 234.1557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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