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 52664U 26145.38618980 +.00000000 +00000-0 +64861-5 0 00007
2 52664 53.2114 169.8166 0001281 112.5905 247.5223 15.08841343 05
| Epoch (UTC): | 25 May 2026 09:16:06 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.8166° |
| argument of perigee: | 112.5905° |
| revolutions per day: | 15.08841343 |
| mean anomaly at epoch: | 247.5223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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