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 26050.15689712 +.00000000 +00000-0 +21413-3 0 00009
2 00082 38.8556 78.1994 1166909 14.6279 348.5379 12.27860732 03
| Epoch (UTC): | 19 February 2026 03:45:55 |
| Eccentricity: | 0.1166909 |
| inclination: | 38.8556° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 78.1994° |
| argument of perigee: | 14.6279° |
| revolutions per day: | 12.27860732 |
| mean anomaly at epoch: | 348.5379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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