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 67993U 26144.93512896 +.00000000 +00000-0 +34010-3 0 00008
2 67993 43.0055 338.3965 0001458 273.7212 86.3473 15.27591337 06
| Epoch (UTC): | 24 May 2026 22:26:35 |
| Eccentricity: | 0.0001458 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.3965° |
| argument of perigee: | 273.7212° |
| revolutions per day: | 15.27591337 |
| mean anomaly at epoch: | 86.3473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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