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 data is extracted from the following two-line orbital elements,
1 02016U 66013A 25131.73294265 .00000719 00000-0 21305-3 0 9996
2 02016 34.0875 229.6778 1163266 59.0006 311.9697 12.65259296689550
| Epoch (UTC): | 11 May 2025 17:35:26 |
| Eccentricity: | 0.1163266 |
| inclination: | 34.0875° |
| perigee height: | 496 km |
| apogee height: | 2306 km |
| right ascension of ascending node: | 229.6778° |
| argument of perigee: | 59.0006° |
| revolutions per day: | 12.65259296 |
| mean anomaly at epoch: | 311.9697° |
| orbit number at epoch: | 68955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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