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 00045U 60007A 23035.93211140 .00000885 00000-0 24413-3 0 9994
2 00045 66.6955 4.1249 0257935 333.4816 25.3271 14.34042991203818
| Epoch (UTC): | 04 February 2023 22:22:14 |
| Eccentricity: | 0.0257935 |
| inclination: | 66.6955° |
| perigee height: | 593 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 4.1249° |
| argument of perigee: | 333.4816° |
| revolutions per day: | 14.34042991 |
| mean anomaly at epoch: | 25.3271° |
| orbit number at epoch: | 20381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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