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 57169U 26145.59951095 +.00000000 +00000-0 +34517-3 0 00005
2 57169 97.5126 207.0967 0010691 171.4456 188.6965 15.23751008 01
| Epoch (UTC): | 25 May 2026 14:23:17 |
| Eccentricity: | 0.0010691 |
| inclination: | 97.5126° |
| perigee height: | 487 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 207.0967° |
| argument of perigee: | 171.4456° |
| revolutions per day: | 15.23751008 |
| mean anomaly at epoch: | 188.6965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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