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 52912U 26145.67476296 +.00000000 +00000-0 +76393-4 0 00009
2 52912 97.8306 34.1094 0001017 113.4523 246.6797 14.79991807 09
| Epoch (UTC): | 25 May 2026 16:11:39 |
| Eccentricity: | 0.0001017 |
| inclination: | 97.8306° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 34.1094° |
| argument of perigee: | 113.4523° |
| revolutions per day: | 14.79991807 |
| mean anomaly at epoch: | 246.6797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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