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 32953U 08025A 23148.08402525 .00000051 00000-0 29363-3 0 9993
2 32953 82.5020 329.6028 0018903 226.6507 133.2998 12.43124148681156
| Epoch (UTC): | 28 May 2023 02:00:59 |
| Eccentricity: | 0.0018903 |
| inclination: | 82.5020° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 329.6028° |
| argument of perigee: | 226.6507° |
| revolutions per day: | 12.43124148 |
| mean anomaly at epoch: | 133.2998° |
| orbit number at epoch: | 68115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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