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 data is extracted from the following two-line orbital elements,
1 32953U 08025A 25139.55793825 .00000041 00000-0 22463-3 0 9996
2 32953 82.5037 240.2480 0020540 92.9691 267.3739 12.43164339770788
| Epoch (UTC): | 19 May 2025 13:23:25 |
| Eccentricity: | 0.0020540 |
| inclination: | 82.5037° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 240.2480° |
| argument of perigee: | 92.9691° |
| revolutions per day: | 12.43164339 |
| mean anomaly at epoch: | 267.3739° |
| orbit number at epoch: | 77078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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