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 23090.86071086 .00016893 00000-0 12873-2 0 9999
2 32788 97.5575 72.1259 0004508 242.4360 117.6407 15.02110725811596
| Epoch (UTC): | 31 March 2023 20:39:25 |
| Eccentricity: | 0.0004508 |
| inclination: | 97.5575° |
| perigee height: | 557 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 72.1259° |
| argument of perigee: | 242.4360° |
| revolutions per day: | 15.02110725 |
| mean anomaly at epoch: | 117.6407° |
| orbit number at epoch: | 81159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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