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 23265.38683993 .00055011 00000-0 90423-2 0 9993
2 00085 38.7571 6.5062 0309283 233.6651 123.5181 14.42785532101325
| Epoch (UTC): | 22 September 2023 09:17:02 |
| Eccentricity: | 0.0309283 |
| inclination: | 38.7571° |
| perigee height: | 529 km |
| apogee height: | 970 km |
| right ascension of ascending node: | 6.5062° |
| argument of perigee: | 233.6651° |
| revolutions per day: | 14.42785532 |
| mean anomaly at epoch: | 123.5181° |
| orbit number at epoch: | 10132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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