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 26161.53535471 +.00000000 +00000-0 +40503-4 0 00004
2 16612 82.5157 95.4558 0018191 112.8106 247.5035 14.86754603 01
| Epoch (UTC): | 10 June 2026 12:50:54 |
| Eccentricity: | 0.0018191 |
| inclination: | 82.5157° |
| perigee height: | 595 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 95.4558° |
| argument of perigee: | 112.8106° |
| revolutions per day: | 14.86754603 |
| mean anomaly at epoch: | 247.5035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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