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 67043U 26145.49166170 +.00000000 +00000-0 +96262-3 0 00003
2 67043 43.0010 324.4670 0000646 268.1881 91.8897 15.27609646 04
| Epoch (UTC): | 25 May 2026 11:47:59 |
| Eccentricity: | 0.0000646 |
| inclination: | 43.0010° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 324.4670° |
| argument of perigee: | 268.1881° |
| revolutions per day: | 15.27609646 |
| mean anomaly at epoch: | 91.8897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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