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 39761U 26104.18821838 +.00000000 +00000-0 +45191-3 0 00004
2 39761 82.4460 148.8193 0019269 215.2016 144.7792 12.42875780 08
| Epoch (UTC): | 14 April 2026 04:31:02 |
| Eccentricity: | 0.0019269 |
| inclination: | 82.4460° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 148.8193° |
| argument of perigee: | 215.2016° |
| revolutions per day: | 12.42875780 |
| mean anomaly at epoch: | 144.7792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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