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 40069U 14037A 23333.83352659 .00000294 00000-0 15527-3 0 9997
2 40069 98.4284 332.1569 0005054 211.2595 148.8283 14.20849513487172
| Epoch (UTC): | 29 November 2023 20:00:16 |
| Eccentricity: | 0.0005054 |
| inclination: | 98.4284° |
| perigee height: | 819 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 332.1569° |
| argument of perigee: | 211.2595° |
| revolutions per day: | 14.20849513 |
| mean anomaly at epoch: | 148.8283° |
| orbit number at epoch: | 48717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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