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 53179U 26145.38153888 +.00000000 +00000-0 +61916-4 0 00007
2 53179 53.2123 139.4370 0000851 59.1720 300.9356 15.08842090 01
| Epoch (UTC): | 25 May 2026 09:09:24 |
| Eccentricity: | 0.0000851 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 139.4370° |
| argument of perigee: | 59.1720° |
| revolutions per day: | 15.08842090 |
| mean anomaly at epoch: | 300.9356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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