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 01642U 65082D 23341.56308859 .00001135 00000-0 13764-3 0 9995
2 01642 32.0947 65.9196 0024671 0.9321 359.1372 14.80900291100523
| Epoch (UTC): | 07 December 2023 13:30:50 |
| Eccentricity: | 0.0024671 |
| inclination: | 32.0947° |
| perigee height: | 609 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 65.9196° |
| argument of perigee: | 0.9321° |
| revolutions per day: | 14.80900291 |
| mean anomaly at epoch: | 359.1372° |
| orbit number at epoch: | 10052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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