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 00116U 61015A 23084.88659281 .00000121 00000-0 15203-3 0 9993
2 00116 66.8079 255.4916 0073960 14.9546 345.3697 13.91898031132558
| Epoch (UTC): | 25 March 2023 21:16:41 |
| Eccentricity: | 0.0073960 |
| inclination: | 66.8079° |
| perigee height: | 868 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 255.4916° |
| argument of perigee: | 14.9546° |
| revolutions per day: | 13.91898031 |
| mean anomaly at epoch: | 345.3697° |
| orbit number at epoch: | 13255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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