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 33066U 08031G 24284.18199578 .00003316 00000-0 55711-3 0 9993
2 33066 48.4405 203.4134 0007635 258.4184 101.5871 14.71740596875776
| Epoch (UTC): | 10 October 2024 04:22:04 |
| Eccentricity: | 0.0007635 |
| inclination: | 48.4405° |
| perigee height: | 650 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 203.4134° |
| argument of perigee: | 258.4184° |
| revolutions per day: | 14.71740596 |
| mean anomaly at epoch: | 101.5871° |
| orbit number at epoch: | 87577 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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