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 11427U 26160.25711412 +.00000000 +00000-0 +60239-4 0 00000
2 11427 74.0160 103.1801 0019676 181.3790 178.7314 14.38886525 08
| Epoch (UTC): | 09 June 2026 06:10:14 |
| Eccentricity: | 0.0019676 |
| inclination: | 74.0160° |
| perigee height: | 748 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 103.1801° |
| argument of perigee: | 181.3790° |
| revolutions per day: | 14.38886525 |
| mean anomaly at epoch: | 178.7314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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