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 22027.06935416 -.00000025 00000-0 20714-4 0 9995
2 00045 66.6938 269.6457 0261918 247.7867 109.5260 14.33770790150219
| Epoch (UTC): | 27 January 2022 01:39:52 |
| Eccentricity: | 0.0261918 |
| inclination: | 66.6938° |
| perigee height: | 591 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 269.6457° |
| argument of perigee: | 247.7867° |
| revolutions per day: | 14.33770790 |
| mean anomaly at epoch: | 109.5260° |
| orbit number at epoch: | 15021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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