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 00011U 59001A 23080.48182127 .00003603 00000-0 19103-2 0 9991
2 00011 32.8664 232.8581 1462118 179.0775 181.2992 11.86815617394564
| Epoch (UTC): | 21 March 2023 11:33:49 |
| Eccentricity: | 0.1462118 |
| inclination: | 32.8664° |
| perigee height: | 553 km |
| apogee height: | 2927 km |
| right ascension of ascending node: | 232.8581° |
| argument of perigee: | 179.0775° |
| revolutions per day: | 11.86815617 |
| mean anomaly at epoch: | 181.2992° |
| orbit number at epoch: | 39456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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