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 67461U 26145.33229584 +.00000000 +00000-0 +92186-3 0 00000
2 67461 42.9984 132.3951 0001370 269.3077 90.7618 15.27604353 08
| Epoch (UTC): | 25 May 2026 07:58:30 |
| Eccentricity: | 0.0001370 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3951° |
| argument of perigee: | 269.3077° |
| revolutions per day: | 15.27604353 |
| mean anomaly at epoch: | 90.7618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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