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 68004U 26145.54673662 +.00000000 +00000-0 +71210-3 0 00002
2 68004 42.9952 335.2350 0000411 316.7647 43.3173 15.27601324 04
| Epoch (UTC): | 25 May 2026 13:07:18 |
| Eccentricity: | 0.0000411 |
| inclination: | 42.9952° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 335.2350° |
| argument of perigee: | 316.7647° |
| revolutions per day: | 15.27601324 |
| mean anomaly at epoch: | 43.3173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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