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 67601U 26145.45879435 +.00000000 +00000-0 +49626-3 0 00006
2 67601 97.2850 210.6502 0000190 196.3958 163.7279 15.33459114 01
| Epoch (UTC): | 25 May 2026 11:00:39 |
| Eccentricity: | 0.0000190 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.6502° |
| argument of perigee: | 196.3958° |
| revolutions per day: | 15.33459114 |
| mean anomaly at epoch: | 163.7279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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