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 52672U 26145.36042698 +.00000000 +00000-0 +21370-4 0 00008
2 52672 53.2124 169.9323 0001211 78.9752 281.1376 15.08837835 03
| Epoch (UTC): | 25 May 2026 08:39:00 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.9323° |
| argument of perigee: | 78.9752° |
| revolutions per day: | 15.08837835 |
| mean anomaly at epoch: | 281.1376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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