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 00107U 61013A 23027.40004391 .00006115 00000-0 79430-3 0 9993
2 00107 28.7876 188.5708 0537615 193.5254 165.0378 14.11204833100942
| Epoch (UTC): | 27 January 2023 09:36:03 |
| Eccentricity: | 0.0537615 |
| inclination: | 28.7876° |
| perigee height: | 466 km |
| apogee height: | 1244 km |
| right ascension of ascending node: | 188.5708° |
| argument of perigee: | 193.5254° |
| revolutions per day: | 14.11204833 |
| mean anomaly at epoch: | 165.0378° |
| orbit number at epoch: | 10094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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