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 67650U 26145.36460819 +.00000000 +00000-0 +31854-3 0 00006
2 67650 97.2851 178.6212 0001145 92.5261 267.6113 15.33444244 01
| Epoch (UTC): | 25 May 2026 08:45:02 |
| Eccentricity: | 0.0001145 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6212° |
| argument of perigee: | 92.5261° |
| revolutions per day: | 15.33444244 |
| mean anomaly at epoch: | 267.6113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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