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 52382U 26145.44486565 +.00000000 +00000-0 +68063-2 0 00008
2 52382 53.2122 201.1703 0000825 103.0974 257.0117 15.25122518 05
| Epoch (UTC): | 25 May 2026 10:40:36 |
| Eccentricity: | 0.0000825 |
| inclination: | 53.2122° |
| perigee height: | 490 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 201.1703° |
| argument of perigee: | 103.0974° |
| revolutions per day: | 15.25122518 |
| mean anomaly at epoch: | 257.0117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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