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 39497U 26032.52657483 +.00000000 +00000-0 +19632-3 0 00002
2 39497 82.4816 252.8332 0013512 29.4296 330.7542 12.43494523 03
| Epoch (UTC): | 01 February 2026 12:38:16 |
| Eccentricity: | 0.0013512 |
| inclination: | 82.4816° |
| perigee height: | 1481 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 252.8332° |
| argument of perigee: | 29.4296° |
| revolutions per day: | 12.43494523 |
| mean anomaly at epoch: | 330.7542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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