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 25109.44029948 .00339152 00000-0 23902-2 0 9997
2 32788 97.6004 105.4654 0009138 131.0434 229.1620 15.73053822925428
| Epoch (UTC): | 19 April 2025 10:34:01 |
| Eccentricity: | 0.0009138 |
| inclination: | 97.6004° |
| perigee height: | 344 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 105.4654° |
| argument of perigee: | 131.0434° |
| revolutions per day: | 15.73053822 |
| mean anomaly at epoch: | 229.1620° |
| orbit number at epoch: | 92542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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