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 16986U 26108.80536551 +.00000000 +00000-0 +24707-3 0 00006
2 16986 82.5282 197.8268 0006637 75.0489 285.1488 15.34269506 02
| Epoch (UTC): | 18 April 2026 19:19:43 |
| Eccentricity: | 0.0006637 |
| inclination: | 82.5282° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 197.8268° |
| argument of perigee: | 75.0489° |
| revolutions per day: | 15.34269506 |
| mean anomaly at epoch: | 285.1488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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