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 67409U 26145.38722973 +.00000000 +00000-0 +49251-3 0 00002
2 67409 43.0020 165.0713 0002107 263.2815 96.7797 15.27592531 02
| Epoch (UTC): | 25 May 2026 09:17:36 |
| Eccentricity: | 0.0002107 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 165.0713° |
| argument of perigee: | 263.2815° |
| revolutions per day: | 15.27592531 |
| mean anomaly at epoch: | 96.7797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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