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 26072.60873595 +.00000000 +00000-0 +27556-3 0 00001
2 39161 97.7417 130.1191 0007399 336.6791 23.4085 14.81087971 04
| Epoch (UTC): | 13 March 2026 14:36:34 |
| Eccentricity: | 0.0007399 |
| inclination: | 97.7417° |
| perigee height: | 621 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 130.1191° |
| argument of perigee: | 336.6791° |
| revolutions per day: | 14.81087971 |
| mean anomaly at epoch: | 23.4085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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