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 67034U 26145.50578826 +.00000000 +00000-0 +85772-3 0 00004
2 67034 43.0012 324.5708 0002192 272.4229 87.6372 15.27602040 03
| Epoch (UTC): | 25 May 2026 12:08:20 |
| Eccentricity: | 0.0002192 |
| inclination: | 43.0012° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.5708° |
| argument of perigee: | 272.4229° |
| revolutions per day: | 15.27602040 |
| mean anomaly at epoch: | 87.6372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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