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 67114U 26144.92532890 +.00000000 +00000-0 +66032-3 0 00007
2 67114 42.9987 98.6094 0000583 264.6744 95.4041 15.27602016 08
| Epoch (UTC): | 24 May 2026 22:12:28 |
| Eccentricity: | 0.0000583 |
| inclination: | 42.9987° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 98.6094° |
| argument of perigee: | 264.6744° |
| revolutions per day: | 15.27602016 |
| mean anomaly at epoch: | 95.4041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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