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 68691U 26141.09350872 +.00000000 +00000-0 +28499-3 0 00006
2 68691 97.6617 216.6604 0013394 151.8197 208.3759 15.08617800 05
| Epoch (UTC): | 21 May 2026 02:14:39 |
| Eccentricity: | 0.0013394 |
| inclination: | 97.6617° |
| perigee height: | 531 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 216.6604° |
| argument of perigee: | 151.8197° |
| revolutions per day: | 15.08617800 |
| mean anomaly at epoch: | 208.3759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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