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 00085U 61004C 22024.84530700 .00003665 00000-0 78601-3 0 9996
2 00085 38.7638 264.6161 0373963 94.6416 269.7134 14.23692645 14589
| Epoch (UTC): | 24 January 2022 20:17:14 |
| Eccentricity: | 0.0373963 |
| inclination: | 38.7638° |
| perigee height: | 544 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 264.6161° |
| argument of perigee: | 94.6416° |
| revolutions per day: | 14.23692645 |
| mean anomaly at epoch: | 269.7134° |
| orbit number at epoch: | 1458 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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