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 67422U 26145.34611641 +.00000000 +00000-0 +48876-3 0 00004
2 67422 43.0025 164.7601 0001003 268.5552 91.5185 15.27590261 06
| Epoch (UTC): | 25 May 2026 08:18:24 |
| Eccentricity: | 0.0001003 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.7601° |
| argument of perigee: | 268.5552° |
| revolutions per day: | 15.27590261 |
| mean anomaly at epoch: | 91.5185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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