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 67152U 26145.51626661 +.00000000 +00000-0 +46642-3 0 00000
2 67152 51.8964 78.3765 0000865 82.1660 277.9401 14.79936263 04
| Epoch (UTC): | 25 May 2026 12:23:25 |
| Eccentricity: | 0.0000865 |
| inclination: | 51.8964° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 78.3765° |
| argument of perigee: | 82.1660° |
| revolutions per day: | 14.79936263 |
| mean anomaly at epoch: | 277.9401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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