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 68005U 26144.95054869 +.00000000 +00000-0 +62069-3 0 00001
2 68005 43.0027 338.4948 0001657 275.4579 84.6084 15.27588011 02
| Epoch (UTC): | 24 May 2026 22:48:47 |
| Eccentricity: | 0.0001657 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4948° |
| argument of perigee: | 275.4579° |
| revolutions per day: | 15.27588011 |
| mean anomaly at epoch: | 84.6084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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