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 68047U 26145.12723691 +.00000000 +00000-0 +22017-3 0 00002
2 68047 53.1592 54.6528 0001125 98.2142 261.8987 15.31040047 03
| Epoch (UTC): | 25 May 2026 03:03:13 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1592° |
| perigee height: | 472 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 54.6528° |
| argument of perigee: | 98.2142° |
| revolutions per day: | 15.31040047 |
| mean anomaly at epoch: | 261.8987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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