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 60116U 26145.42589933 +.00000000 +00000-0 -67524-5 0 00008
2 60116 53.1591 203.1216 0001228 109.5803 250.5348 15.69693612 09
| Epoch (UTC): | 25 May 2026 10:13:17 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 203.1216° |
| argument of perigee: | 109.5803° |
| revolutions per day: | 15.69693612 |
| mean anomaly at epoch: | 250.5348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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