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 60017U 26145.51167463 +.00000000 +00000-0 +20900-4 0 00003
2 60017 53.1619 78.9145 0001129 90.6179 269.4952 15.31702764 03
| Epoch (UTC): | 25 May 2026 12:16:48 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.1619° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.9145° |
| argument of perigee: | 90.6179° |
| revolutions per day: | 15.31702764 |
| mean anomaly at epoch: | 269.4952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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