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 32788U 08021F 25132.88231804 .00919871 39972-3 19863-2 0 9993
2 32788 97.5876 131.4358 0009092 159.3385 200.8261 15.98424668929137
| Epoch (UTC): | 12 May 2025 21:10:32 |
| Eccentricity: | 0.0009092 |
| inclination: | 97.5876° |
| perigee height: | 273 km |
| apogee height: | 285 km |
| right ascension of ascending node: | 131.4358° |
| argument of perigee: | 159.3385° |
| revolutions per day: | 15.98424668 |
| mean anomaly at epoch: | 200.8261° |
| orbit number at epoch: | 92913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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