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 61867U 26145.52316564 +.00000000 +00000-0 +24084-4 0 00003
2 61867 43.0007 164.4727 0001657 270.2004 89.8658 15.27579769 01
| Epoch (UTC): | 25 May 2026 12:33:21 |
| Eccentricity: | 0.0001657 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.4727° |
| argument of perigee: | 270.2004° |
| revolutions per day: | 15.27579769 |
| mean anomaly at epoch: | 89.8658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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