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 27432U 02024C 23028.60403434 .00000048 00000-0 48601-4 0 9990
2 27432 99.0414 61.6600 0050354 2.0532 108.9412 14.14176542 68649
| Epoch (UTC): | 28 January 2023 14:29:48 |
| Eccentricity: | 0.0050354 |
| inclination: | 99.0414° |
| perigee height: | 809 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 61.6600° |
| argument of perigee: | 2.0532° |
| revolutions per day: | 14.14176542 |
| mean anomaly at epoch: | 108.9412° |
| orbit number at epoch: | 6864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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