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 27004U 01056D 23083.43338248 .00000056 00000-0 11529-3 0 9998
2 27004 99.6643 229.4104 0019076 292.8741 137.4037 13.70171935 64484
| Epoch (UTC): | 24 March 2023 10:24:04 |
| Eccentricity: | 0.0019076 |
| inclination: | 99.6643° |
| perigee height: | 985 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 229.4104° |
| argument of perigee: | 292.8741° |
| revolutions per day: | 13.70171935 |
| mean anomaly at epoch: | 137.4037° |
| orbit number at epoch: | 6448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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