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 06324U 72104B 23152.12315506 .00000303 00000-0 96618-4 0 9995
2 06324 74.0790 34.4734 0009290 327.4696 32.5888 14.43932783649137
| Epoch (UTC): | 01 June 2023 02:57:20 |
| Eccentricity: | 0.0009290 |
| inclination: | 74.0790° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 34.4734° |
| argument of perigee: | 327.4696° |
| revolutions per day: | 14.43932783 |
| mean anomaly at epoch: | 32.5888° |
| orbit number at epoch: | 64913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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