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 26106.92514575 +.00000000 +00000-0 +10558-2 0 00003
2 39761 82.4454 147.1050 0019377 209.1030 150.8971 12.42876265 09
| Epoch (UTC): | 16 April 2026 22:12:12 |
| Eccentricity: | 0.0019377 |
| inclination: | 82.4454° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 147.1050° |
| argument of perigee: | 209.1030° |
| revolutions per day: | 12.42876265 |
| mean anomaly at epoch: | 150.8971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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