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 16612U 26159.31437692 +.00000000 +00000-0 +50707-4 0 00000
2 16612 82.5155 97.5483 0018104 119.5897 240.7127 14.86753039 03
| Epoch (UTC): | 08 June 2026 07:32:42 |
| Eccentricity: | 0.0018104 |
| inclination: | 82.5155° |
| perigee height: | 595 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 97.5483° |
| argument of perigee: | 119.5897° |
| revolutions per day: | 14.86753039 |
| mean anomaly at epoch: | 240.7127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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