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 14064U 83044A 23155.62164727 .00003032 00000-0 22432-3 0 9999
2 14064 64.9999 7.6750 0108485 262.6475 96.2305 15.00584380 49008
| Epoch (UTC): | 04 June 2023 14:55:10 |
| Eccentricity: | 0.0108485 |
| inclination: | 64.9999° |
| perigee height: | 490 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 7.6750° |
| argument of perigee: | 262.6475° |
| revolutions per day: | 15.00584380 |
| mean anomaly at epoch: | 96.2305° |
| orbit number at epoch: | 4900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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