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 23464U 95002B 23082.73178561 .00000199 00000-0 19921-3 0 9992
2 23464 82.9312 172.6162 0041062 189.6650 170.3720 13.72719429410403
| Epoch (UTC): | 23 March 2023 17:33:46 |
| Eccentricity: | 0.0041062 |
| inclination: | 82.9312° |
| perigee height: | 959 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 172.6162° |
| argument of perigee: | 189.6650° |
| revolutions per day: | 13.72719429 |
| mean anomaly at epoch: | 170.3720° |
| orbit number at epoch: | 41040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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