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 68240U 26144.64861238 +.00000000 +00000-0 +45673-3 0 00006
2 68240 53.1586 301.7963 0001280 35.3054 324.8036 15.42161466 02
| Epoch (UTC): | 24 May 2026 15:34:00 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.1586° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 301.7963° |
| argument of perigee: | 35.3054° |
| revolutions per day: | 15.42161466 |
| mean anomaly at epoch: | 324.8036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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