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 26162.54488919 +.00000000 +00000-0 +40585-4 0 00000
2 16612 82.5159 94.5047 0018232 109.7352 250.5834 14.86755420 09
| Epoch (UTC): | 11 June 2026 13:04:38 |
| Eccentricity: | 0.0018232 |
| inclination: | 82.5159° |
| perigee height: | 595 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 94.5047° |
| argument of perigee: | 109.7352° |
| revolutions per day: | 14.86755420 |
| mean anomaly at epoch: | 250.5834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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