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 68839U 26145.58335647 +.00000000 +00000-0 +31398-3 0 00003
2 68839 97.2857 160.2006 0001670 95.5431 300.7477 15.49177108 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001670 |
| inclination: | 97.2857° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.2006° |
| argument of perigee: | 95.5431° |
| revolutions per day: | 15.49177108 |
| mean anomaly at epoch: | 300.7477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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