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 21128.84005463 -.00000059 00000-0 -39848-4 0 9994
2 00012 32.9041 292.4314 1666476 346.7498 9.3983 11.44399255317260
| Epoch (UTC): | 08 May 2021 20:09:40 |
| Eccentricity: | 0.1666476 |
| inclination: | 32.9041° |
| perigee height: | 553 km |
| apogee height: | 3326 km |
| right ascension of ascending node: | 292.4314° |
| argument of perigee: | 346.7498° |
| revolutions per day: | 11.44399255 |
| mean anomaly at epoch: | 9.3983° |
| orbit number at epoch: | 31726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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