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 52665U 26145.36778464 +.00000000 +00000-0 -15825-3 0 00005
2 52665 53.2124 169.8991 0000938 78.0960 282.0137 15.08855065 02
| Epoch (UTC): | 25 May 2026 08:49:36 |
| Eccentricity: | 0.0000938 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.8991° |
| argument of perigee: | 78.0960° |
| revolutions per day: | 15.08855065 |
| mean anomaly at epoch: | 282.0137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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