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 67680U 26145.59617441 +.00000000 +00000-0 +38142-3 0 00006
2 67680 96.6168 212.0685 0021025 197.8067 162.2438 15.24820635 09
| Epoch (UTC): | 25 May 2026 14:18:29 |
| Eccentricity: | 0.0021025 |
| inclination: | 96.6168° |
| perigee height: | 477 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 212.0685° |
| argument of perigee: | 197.8067° |
| revolutions per day: | 15.24820635 |
| mean anomaly at epoch: | 162.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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