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 39763U 26053.83936567 +.00000000 +00000-0 +40428-3 0 00005
2 39763 82.4500 180.5170 0020178 324.3230 35.6500 12.42976164 07
| Epoch (UTC): | 22 February 2026 20:08:41 |
| Eccentricity: | 0.0020178 |
| inclination: | 82.4500° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 180.5170° |
| argument of perigee: | 324.3230° |
| revolutions per day: | 12.42976164 |
| mean anomaly at epoch: | 35.6500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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