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 16116U 26138.60296419 +.00000000 +00000-0 +00000-0 0 00005
2 16116 14.3840 347.6601 0001560 240.5207 95.3544 0.99322745 07
| Epoch (UTC): | 18 May 2026 14:28:16 |
| Eccentricity: | 0.0001560 |
| inclination: | 14.3840° |
| perigee height: | 36048 km |
| apogee height: | 36061 km |
| right ascension of ascending node: | 347.6601° |
| argument of perigee: | 240.5207° |
| revolutions per day: | 0.99322745 |
| mean anomaly at epoch: | 95.3544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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