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 67455U 26145.38227127 +.00000000 +00000-0 +95435-4 0 00000
2 67455 42.9996 131.9108 0001472 270.3497 89.7186 15.27560412 09
| Epoch (UTC): | 25 May 2026 09:10:28 |
| Eccentricity: | 0.0001472 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.9108° |
| argument of perigee: | 270.3497° |
| revolutions per day: | 15.27560412 |
| mean anomaly at epoch: | 89.7186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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