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 23908U 96029C 23087.74899115 0.00002500 00000-0 65997-3 0 01
2 23908 63.3394 13.6634 0785247 32.6693 327.3307 13.41564476 03
| Epoch (UTC): | 28 March 2023 17:58:32 |
| Eccentricity: | 0.0785247 |
| inclination: | 63.3394° |
| perigee height: | 516 km |
| apogee height: | 1691 km |
| right ascension of ascending node: | 13.6634° |
| argument of perigee: | 32.6693° |
| revolutions per day: | 13.41564476 |
| mean anomaly at epoch: | 327.3307° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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