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 25520U 98064B 23083.15157496 .00025496 00000-0 73127-3 0 9994
2 25520 28.4422 8.1540 0004334 7.2965 352.7694 15.34474385357116
| Epoch (UTC): | 24 March 2023 03:38:16 |
| Eccentricity: | 0.0004334 |
| inclination: | 28.4422° |
| perigee height: | 459 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 8.1540° |
| argument of perigee: | 7.2965° |
| revolutions per day: | 15.34474385 |
| mean anomaly at epoch: | 352.7694° |
| orbit number at epoch: | 35711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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