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 67424U 26145.43719993 +.00000000 +00000-0 +47236-3 0 00004
2 67424 43.0025 164.5847 0001628 263.8910 96.1757 15.27591298 04
| Epoch (UTC): | 25 May 2026 10:29:34 |
| Eccentricity: | 0.0001628 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5847° |
| argument of perigee: | 263.8910° |
| revolutions per day: | 15.27591298 |
| mean anomaly at epoch: | 96.1757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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