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 27464U 02036A 23088.47738071 .00000035 00000-0 17746-3 0 9998
2 27464 82.4901 0.0769 0024890 312.7875 47.1116 12.44586700941569
| Epoch (UTC): | 29 March 2023 11:27:25 |
| Eccentricity: | 0.0024890 |
| inclination: | 82.4901° |
| perigee height: | 1467 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 0.0769° |
| argument of perigee: | 312.7875° |
| revolutions per day: | 12.44586700 |
| mean anomaly at epoch: | 47.1116° |
| orbit number at epoch: | 94156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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