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 52670U 26145.44139808 +.00000000 +00000-0 -41150-5 0 00005
2 52670 53.2103 169.6370 0001151 59.9654 300.1452 15.08842142 04
| Epoch (UTC): | 25 May 2026 10:35:36 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.2103° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.6370° |
| argument of perigee: | 59.9654° |
| revolutions per day: | 15.08842142 |
| mean anomaly at epoch: | 300.1452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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