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 25138.83362601 .00000036 00000-0 18752-3 0 9990
2 32953 82.5036 240.6984 0020546 94.4705 265.8722 12.43164287770832
| Epoch (UTC): | 18 May 2025 20:00:25 |
| Eccentricity: | 0.0020546 |
| inclination: | 82.5036° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 240.6984° |
| argument of perigee: | 94.4705° |
| revolutions per day: | 12.43164287 |
| mean anomaly at epoch: | 265.8722° |
| orbit number at epoch: | 77083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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