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 68765U 26110.15512012 +.00000000 +00000-0 +17840-3 0 00005
2 68765 42.9612 171.3926 0162582 193.6002 166.0453 15.64310274 00
| Epoch (UTC): | 20 April 2026 03:43:22 |
| Eccentricity: | 0.0162582 |
| inclination: | 42.9612° |
| perigee height: | 265 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 171.3926° |
| argument of perigee: | 193.6002° |
| revolutions per day: | 15.64310274 |
| mean anomaly at epoch: | 166.0453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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