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 39442U 13066AC 23331.91748027 .00011981 00000-0 98497-3 0 9998
2 39442 97.4901 317.6454 0023885 285.5510 74.3076 14.99067141543153
| Epoch (UTC): | 27 November 2023 22:01:10 |
| Eccentricity: | 0.0023885 |
| inclination: | 97.4901° |
| perigee height: | 553 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 317.6454° |
| argument of perigee: | 285.5510° |
| revolutions per day: | 14.99067141 |
| mean anomaly at epoch: | 74.3076° |
| orbit number at epoch: | 54315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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