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 67421U 26145.45904995 +.00000000 +00000-0 +40525-3 0 00005
2 67421 43.0001 164.7529 0001678 275.6932 84.3728 15.27593218 05
| Epoch (UTC): | 25 May 2026 11:01:01 |
| Eccentricity: | 0.0001678 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.7529° |
| argument of perigee: | 275.6932° |
| revolutions per day: | 15.27593218 |
| mean anomaly at epoch: | 84.3728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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