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 34476U 93036TV 23333.80382926 .00008233 00000-0 60062-2 0 9999
2 34476 74.0144 244.3883 0353492 262.8479 93.2331 13.70341685734016
| Epoch (UTC): | 29 November 2023 19:17:30 |
| Eccentricity: | 0.0353492 |
| inclination: | 74.0144° |
| perigee height: | 737 km |
| apogee height: | 1259 km |
| right ascension of ascending node: | 244.3883° |
| argument of perigee: | 262.8479° |
| revolutions per day: | 13.70341685 |
| mean anomaly at epoch: | 93.2331° |
| orbit number at epoch: | 73401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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