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 67423U 26145.45136067 +.00000000 +00000-0 +13429-2 0 00006
2 67423 43.0018 164.6970 0001793 256.1900 103.8753 15.27589295 06
| Epoch (UTC): | 25 May 2026 10:49:57 |
| Eccentricity: | 0.0001793 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.6970° |
| argument of perigee: | 256.1900° |
| revolutions per day: | 15.27589295 |
| mean anomaly at epoch: | 103.8753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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