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 5104U 71024A 23334.46190888 .00000023 00000-0 65593-4 0 9990
2 5104 88.1593 104.9456 0042314 262.5009 166.1090 12.67861427437217
| Epoch (UTC): | 30 November 2023 11:05:08 |
| Eccentricity: | 0.0042314 |
| inclination: | 88.1593° |
| perigee height: | 1358 km |
| apogee height: | 1423 km |
| right ascension of ascending node: | 104.9456° |
| argument of perigee: | 262.5009° |
| revolutions per day: | 12.67861427 |
| mean anomaly at epoch: | 166.1090° |
| orbit number at epoch: | 43721 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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