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 39058U 13001B 23083.79941328 .00000024 00000-0 10070-3 0 9996
2 39058 82.4977 230.5339 0017267 74.7498 285.5484 12.43977472462522
| Epoch (UTC): | 24 March 2023 19:11:09 |
| Eccentricity: | 0.0017267 |
| inclination: | 82.4977° |
| perigee height: | 1476 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 230.5339° |
| argument of perigee: | 74.7498° |
| revolutions per day: | 12.43977472 |
| mean anomaly at epoch: | 285.5484° |
| orbit number at epoch: | 46252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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