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 23032.52678786 .00012000 00000-0 22689-2 0 9995
2 00085 38.7629 143.4084 0359218 82.9826 281.1630 14.30142521 67846
| Epoch (UTC): | 01 February 2023 12:38:34 |
| Eccentricity: | 0.0359218 |
| inclination: | 38.7629° |
| perigee height: | 534 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 143.4084° |
| argument of perigee: | 82.9826° |
| revolutions per day: | 14.30142521 |
| mean anomaly at epoch: | 281.1630° |
| orbit number at epoch: | 6784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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