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 26066.12298744 +.00000000 +00000-0 +27414-3 0 00001
2 39161 97.7420 123.8542 0007921 358.8724 1.2470 14.81056515 02
| Epoch (UTC): | 07 March 2026 02:57:06 |
| Eccentricity: | 0.0007921 |
| inclination: | 97.7420° |
| perigee height: | 620 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 123.8542° |
| argument of perigee: | 358.8724° |
| revolutions per day: | 14.81056515 |
| mean anomaly at epoch: | 1.2470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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