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 68760U 26139.81967880 +.00000000 +00000-0 +12342-4 0 00004
2 68760 98.2868 214.1067 0002254 150.4995 209.6331 14.57608955 01
| Epoch (UTC): | 19 May 2026 19:40:20 |
| Eccentricity: | 0.0002254 |
| inclination: | 98.2868° |
| perigee height: | 699 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 214.1067° |
| argument of perigee: | 150.4995° |
| revolutions per day: | 14.57608955 |
| mean anomaly at epoch: | 209.6331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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