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 00012U 59001B 23335.19067288 .00000785 00000-0 43718-3 0 9991
2 00012 32.9087 253.0387 1660297 234.6439 108.7634 11.45883848424597
| Epoch (UTC): | 01 December 2023 04:34:34 |
| Eccentricity: | 0.1660297 |
| inclination: | 32.9087° |
| perigee height: | 553 km |
| apogee height: | 3312 km |
| right ascension of ascending node: | 253.0387° |
| argument of perigee: | 234.6439° |
| revolutions per day: | 11.45883848 |
| mean anomaly at epoch: | 108.7634° |
| orbit number at epoch: | 42459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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