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 23091.85992180 .00015612 00000-0 11893-2 0 9995
2 32788 97.5575 73.0998 0004673 238.1383 121.9387 15.02141471811649
| Epoch (UTC): | 01 April 2023 20:38:17 |
| Eccentricity: | 0.0004673 |
| inclination: | 97.5575° |
| perigee height: | 557 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 73.0998° |
| argument of perigee: | 238.1383° |
| revolutions per day: | 15.02141471 |
| mean anomaly at epoch: | 121.9387° |
| orbit number at epoch: | 81164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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