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 32789U 08021G 23161.00226291 .00053707 00000-0 15285-2 0 9990
2 32789 97.3031 182.5404 0009315 139.4372 220.7567 15.35900093826386
| Epoch (UTC): | 10 June 2023 00:03:15 |
| Eccentricity: | 0.0009315 |
| inclination: | 97.3031° |
| perigee height: | 452 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 182.5404° |
| argument of perigee: | 139.4372° |
| revolutions per day: | 15.35900093 |
| mean anomaly at epoch: | 220.7567° |
| orbit number at epoch: | 82638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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