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 33493U 09002B 23157.02854785 .00010307 00000-0 70402-3 0 9997
2 33493 98.2454 170.7672 0018251 86.0413 274.2898 15.06250688782070
| Epoch (UTC): | 06 June 2023 00:41:06 |
| Eccentricity: | 0.0018251 |
| inclination: | 98.2454° |
| perigee height: | 535 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 170.7672° |
| argument of perigee: | 86.0413° |
| revolutions per day: | 15.06250688 |
| mean anomaly at epoch: | 274.2898° |
| orbit number at epoch: | 78207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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