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 26067.57914904 +.00000000 +00000-0 +87554-4 0 00002
2 16612 82.5185 183.9632 0018131 68.5567 291.7582 14.86678703 04
| Epoch (UTC): | 08 March 2026 13:53:58 |
| Eccentricity: | 0.0018131 |
| inclination: | 82.5185° |
| perigee height: | 596 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 183.9632° |
| argument of perigee: | 68.5567° |
| revolutions per day: | 14.86678703 |
| mean anomaly at epoch: | 291.7582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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