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 40074U 14037F 23334.07792256 .00009622 00000-0 99331-3 0 9990
2 40074 98.3384 247.3922 0004800 27.3460 332.8008 14.90394230508940
| Epoch (UTC): | 30 November 2023 01:52:12 |
| Eccentricity: | 0.0004800 |
| inclination: | 98.3384° |
| perigee height: | 593 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 247.3922° |
| argument of perigee: | 27.3460° |
| revolutions per day: | 14.90394230 |
| mean anomaly at epoch: | 332.8008° |
| orbit number at epoch: | 50894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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