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 26104.08976122 +.00000000 +00000-0 +12098-3 0 00004
2 00082 38.8637 237.8751 1167698 275.7393 71.1591 12.27891673 04
| Epoch (UTC): | 14 April 2026 02:09:15 |
| Eccentricity: | 0.1167698 |
| inclination: | 38.8637° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 237.8751° |
| argument of perigee: | 275.7393° |
| revolutions per day: | 12.27891673 |
| mean anomaly at epoch: | 71.1591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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