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 67653U 26145.06280640 +.00000000 +00000-0 +61427-3 0 00007
2 67653 97.2842 178.2684 0000908 93.1417 266.9930 15.33454723 01
| Epoch (UTC): | 25 May 2026 01:30:26 |
| Eccentricity: | 0.0000908 |
| inclination: | 97.2842° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.2684° |
| argument of perigee: | 93.1417° |
| revolutions per day: | 15.33454723 |
| mean anomaly at epoch: | 266.9930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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