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 25188.56963442 .00000040 00000-0 21842-3 0 9994
2 32953 82.5010 209.7717 0018882 348.7087 11.3566 12.43166013776871
| Epoch (UTC): | 07 July 2025 13:40:16 |
| Eccentricity: | 0.0018882 |
| inclination: | 82.5010° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 209.7717° |
| argument of perigee: | 348.7087° |
| revolutions per day: | 12.43166013 |
| mean anomaly at epoch: | 11.3566° |
| orbit number at epoch: | 77687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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