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 32376U 07059A 23150.77749807 .00000501 00000-0 69503-4 0 9995
2 32376 97.8884 334.5063 0001307 93.2780 266.8582 14.82161346837158
| Epoch (UTC): | 30 May 2023 18:39:35 |
| Eccentricity: | 0.0001307 |
| inclination: | 97.8884° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 334.5063° |
| argument of perigee: | 93.2780° |
| revolutions per day: | 14.82161346 |
| mean anomaly at epoch: | 266.8582° |
| orbit number at epoch: | 83715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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