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 26101.11768139 +.00000000 +00000-0 +20541-3 0 00004
2 39161 97.7355 157.6477 0007189 226.3286 133.7332 14.81203955 09
| Epoch (UTC): | 11 April 2026 02:49:27 |
| Eccentricity: | 0.0007189 |
| inclination: | 97.7355° |
| perigee height: | 620 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 157.6477° |
| argument of perigee: | 226.3286° |
| revolutions per day: | 14.81203955 |
| mean anomaly at epoch: | 133.7332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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