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 10011U 77036B 23150.88681340 -.00000051 00000-0 79823-5 0 9996
2 10011 65.8664 81.2385 0692203 109.8738 316.0509 12.32228824 49770
| Epoch (UTC): | 30 May 2023 21:17:00 |
| Eccentricity: | 0.0692203 |
| inclination: | 65.8664° |
| perigee height: | 991 km |
| apogee height: | 2088 km |
| right ascension of ascending node: | 81.2385° |
| argument of perigee: | 109.8738° |
| revolutions per day: | 12.32228824 |
| mean anomaly at epoch: | 316.0509° |
| orbit number at epoch: | 4977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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