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 03373U 65082ML 24357.62181617 .00010648 00000-0 25348-2 0 9993
2 03373 30.9799 78.2082 0166584 81.6324 280.3143 14.44625773972143
| Epoch (UTC): | 22 December 2024 14:55:24 |
| Eccentricity: | 0.0166584 |
| inclination: | 30.9799° |
| perigee height: | 624 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 78.2082° |
| argument of perigee: | 81.6324° |
| revolutions per day: | 14.44625773 |
| mean anomaly at epoch: | 280.3143° |
| orbit number at epoch: | 97214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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