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 53171U 26145.33279748 +.00000000 +00000-0 +23551-4 0 00001
2 53171 53.2112 149.8159 0001071 57.0376 303.0719 15.08842263 09
| Epoch (UTC): | 25 May 2026 07:59:13 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 149.8159° |
| argument of perigee: | 57.0376° |
| revolutions per day: | 15.08842263 |
| mean anomaly at epoch: | 303.0719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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