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 67125U 26145.23940981 +.00000000 +00000-0 +34800-3 0 00006
2 67125 43.0018 96.6630 0000952 268.8552 91.2191 15.27586256 01
| Epoch (UTC): | 25 May 2026 05:44:45 |
| Eccentricity: | 0.0000952 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.6630° |
| argument of perigee: | 268.8552° |
| revolutions per day: | 15.27586256 |
| mean anomaly at epoch: | 91.2191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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