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 67407U 26145.43848791 +.00000000 +00000-0 +57092-3 0 00005
2 67407 43.0022 164.5981 0000980 292.9445 67.1304 15.27589235 01
| Epoch (UTC): | 25 May 2026 10:31:25 |
| Eccentricity: | 0.0000980 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5981° |
| argument of perigee: | 292.9445° |
| revolutions per day: | 15.27589235 |
| mean anomaly at epoch: | 67.1304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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