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 67568U 26145.58405687 +.00000000 +00000-0 +72933-3 0 00003
2 67568 97.2856 205.9882 0000848 327.4164 32.7027 15.33458294 07
| Epoch (UTC): | 25 May 2026 14:01:02 |
| Eccentricity: | 0.0000848 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9882° |
| argument of perigee: | 327.4164° |
| revolutions per day: | 15.33458294 |
| mean anomaly at epoch: | 32.7027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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