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 52692U 26145.33555536 +.00000000 +00000-0 -17286-3 0 00008
2 52692 53.2125 159.7732 0001153 75.5752 284.5368 15.08850344 03
| Epoch (UTC): | 25 May 2026 08:03:11 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.7732° |
| argument of perigee: | 75.5752° |
| revolutions per day: | 15.08850344 |
| mean anomaly at epoch: | 284.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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