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 26161.50263109 +.00000000 +00000-0 +40558-3 0 00006
2 39761 82.4442 112.9176 0021286 92.6218 267.7299 12.42878501 06
| Epoch (UTC): | 10 June 2026 12:03:47 |
| Eccentricity: | 0.0021286 |
| inclination: | 82.4442° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 112.9176° |
| argument of perigee: | 92.6218° |
| revolutions per day: | 12.42878501 |
| mean anomaly at epoch: | 267.7299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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