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 33499U 09002H 23341.57627919 .00001537 00000-0 22147-3 0 9993
2 33499 98.1543 235.9761 0009642 37.6416 322.5467 14.77783132799660
| Epoch (UTC): | 07 December 2023 13:49:50 |
| Eccentricity: | 0.0009642 |
| inclination: | 98.1543° |
| perigee height: | 629 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 235.9761° |
| argument of perigee: | 37.6416° |
| revolutions per day: | 14.77783132 |
| mean anomaly at epoch: | 322.5467° |
| orbit number at epoch: | 79966 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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