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 68327U 26145.57543566 +.00000000 +00000-0 +10740-2 0 00002
2 68327 53.1589 350.7001 0001192 77.0132 283.1002 15.30218305 02
| Epoch (UTC): | 25 May 2026 13:48:37 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.7001° |
| argument of perigee: | 77.0132° |
| revolutions per day: | 15.30218305 |
| mean anomaly at epoch: | 283.1002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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