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 39092U 26156.03021330 +.00000000 +00000-0 +82359-4 0 00009
2 39092 98.4031 335.8751 0007874 273.6688 86.3598 14.36408291 05
| Epoch (UTC): | 05 June 2026 00:43:30 |
| Eccentricity: | 0.0007874 |
| inclination: | 98.4031° |
| perigee height: | 765 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 335.8751° |
| argument of perigee: | 273.6688° |
| revolutions per day: | 14.36408291 |
| mean anomaly at epoch: | 86.3598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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