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 35432U 93036AKA 23334.26484460 .00020999 00000-0 43387-2 0 9993
2 35432 74.0456 45.4619 0012904 299.0926 60.8947 14.60254593764883
| Epoch (UTC): | 30 November 2023 06:21:22 |
| Eccentricity: | 0.0012904 |
| inclination: | 74.0456° |
| perigee height: | 683 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 45.4619° |
| argument of perigee: | 299.0926° |
| revolutions per day: | 14.60254593 |
| mean anomaly at epoch: | 60.8947° |
| orbit number at epoch: | 76488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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