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 25167.16224706 .00000019 00000-0 61885-4 0 9998
2 32953 82.5026 223.0843 0019801 35.2673 324.9713 12.43165263774352
| Epoch (UTC): | 16 June 2025 03:53:38 |
| Eccentricity: | 0.0019801 |
| inclination: | 82.5026° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 223.0843° |
| argument of perigee: | 35.2673° |
| revolutions per day: | 12.43165263 |
| mean anomaly at epoch: | 324.9713° |
| orbit number at epoch: | 77435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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