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 44712U 19039P 23155.84361527 .00002670 00000-0 35982-3 0 9997
2 44712 97.6968 179.5926 0048509 53.0239 307.5399 14.79154546198035
| Epoch (UTC): | 04 June 2023 20:14:48 |
| Eccentricity: | 0.0048509 |
| inclination: | 97.6968° |
| perigee height: | 598 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 179.5926° |
| argument of perigee: | 53.0239° |
| revolutions per day: | 14.79154546 |
| mean anomaly at epoch: | 307.5399° |
| orbit number at epoch: | 19803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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