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 16987U 26109.09755354 +.00000000 +00000-0 +30377-4 0 00004
2 16987 82.5163 164.4465 0018817 60.0016 318.4339 14.85406984 06
| Epoch (UTC): | 19 April 2026 02:20:28 |
| Eccentricity: | 0.0018817 |
| inclination: | 82.5163° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 164.4465° |
| argument of perigee: | 60.0016° |
| revolutions per day: | 14.85406984 |
| mean anomaly at epoch: | 318.4339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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