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 14974U 84046B 23153.56019394 -.00000006 00000-0 -21259-4 0 9999
2 14974 82.9341 323.1206 0045747 32.0682 31.6915 13.76980363961466
| Epoch (UTC): | 02 June 2023 13:26:40 |
| Eccentricity: | 0.0045747 |
| inclination: | 82.9341° |
| perigee height: | 941 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 323.1206° |
| argument of perigee: | 32.0682° |
| revolutions per day: | 13.76980363 |
| mean anomaly at epoch: | 31.6915° |
| orbit number at epoch: | 96146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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