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 67414U 26145.35509409 +.00000000 +00000-0 +42228-3 0 00009
2 67414 43.0055 164.8223 0005322 287.4394 72.5875 15.27566914 06
| Epoch (UTC): | 25 May 2026 08:31:20 |
| Eccentricity: | 0.0005322 |
| inclination: | 43.0055° |
| perigee height: | 479 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 164.8223° |
| argument of perigee: | 287.4394° |
| revolutions per day: | 15.27566914 |
| mean anomaly at epoch: | 72.5875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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