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 39161U 26069.97391593 +.00000000 +00000-0 +28550-3 0 00005
2 39161 97.7418 127.5741 0007618 345.8442 14.2556 14.81076249 02
| Epoch (UTC): | 10 March 2026 23:22:26 |
| Eccentricity: | 0.0007618 |
| inclination: | 97.7418° |
| perigee height: | 621 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 127.5741° |
| argument of perigee: | 345.8442° |
| revolutions per day: | 14.81076249 |
| mean anomaly at epoch: | 14.2556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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