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 27465U 02036B 23084.45790963 .00000004 00000-0 -38029-4 0 9996
2 27465 82.4899 359.6042 0025813 316.9968 42.9094 12.44908024941293
| Epoch (UTC): | 25 March 2023 10:59:23 |
| Eccentricity: | 0.0025813 |
| inclination: | 82.4899° |
| perigee height: | 1465 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 359.6042° |
| argument of perigee: | 316.9968° |
| revolutions per day: | 12.44908024 |
| mean anomaly at epoch: | 42.9094° |
| orbit number at epoch: | 94129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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