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 67458U 26145.43351235 +.00000000 +00000-0 +53166-3 0 00001
2 67458 43.0011 131.4202 0001521 283.5584 76.5099 15.27620790 03
| Epoch (UTC): | 25 May 2026 10:24:15 |
| Eccentricity: | 0.0001521 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.4202° |
| argument of perigee: | 283.5584° |
| revolutions per day: | 15.27620790 |
| mean anomaly at epoch: | 76.5099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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