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 09903U 77024A 23151.91313950 .00000223 00000-0 12206-3 0 9995
2 09903 81.2704 134.0390 0036543 268.7975 90.9008 14.08466981370968
| Epoch (UTC): | 31 May 2023 21:54:55 |
| Eccentricity: | 0.0036543 |
| inclination: | 81.2704° |
| perigee height: | 838 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 134.0390° |
| argument of perigee: | 268.7975° |
| revolutions per day: | 14.08466981 |
| mean anomaly at epoch: | 90.9008° |
| orbit number at epoch: | 37096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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