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 67708U 26145.55027698 +.00000000 +00000-0 +74849-3 0 00006
2 67708 97.2839 257.1893 0000405 118.6030 241.5254 15.33450262 05
| Epoch (UTC): | 25 May 2026 13:12:23 |
| Eccentricity: | 0.0000405 |
| inclination: | 97.2839° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1893° |
| argument of perigee: | 118.6030° |
| revolutions per day: | 15.33450262 |
| mean anomaly at epoch: | 241.5254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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