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 00082U 26106.28639566 +.00000000 +00000-0 +12009-3 0 00008
2 00082 38.8631 229.7175 1167612 286.3619 61.2004 12.27892340 04
| Epoch (UTC): | 16 April 2026 06:52:24 |
| Eccentricity: | 0.1167612 |
| inclination: | 38.8631° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 229.7175° |
| argument of perigee: | 286.3619° |
| revolutions per day: | 12.27892340 |
| mean anomaly at epoch: | 61.2004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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