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 67322U 26145.63792591 +.00000000 +00000-0 +71114-3 0 00000
2 67322 43.0000 251.0101 0001089 284.8828 75.1903 15.27604250 04
| Epoch (UTC): | 25 May 2026 15:18:36 |
| Eccentricity: | 0.0001089 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.0101° |
| argument of perigee: | 284.8828° |
| revolutions per day: | 15.27604250 |
| mean anomaly at epoch: | 75.1903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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