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 68159U 26145.53546709 +.00000000 +00000-0 +60728-3 0 00005
2 68159 97.2853 167.1808 0000923 93.8972 266.2376 15.33462055 04
| Epoch (UTC): | 25 May 2026 12:51:04 |
| Eccentricity: | 0.0000923 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.1808° |
| argument of perigee: | 93.8972° |
| revolutions per day: | 15.33462055 |
| mean anomaly at epoch: | 266.2376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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