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 09023U 76069B 23152.92641254 .00000300 00000-0 10345-3 0 9997
2 09023 74.0446 40.4461 0016821 25.6569 334.5417 14.40021456457641
| Epoch (UTC): | 01 June 2023 22:14:02 |
| Eccentricity: | 0.0016821 |
| inclination: | 74.0446° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 40.4461° |
| argument of perigee: | 25.6569° |
| revolutions per day: | 14.40021456 |
| mean anomaly at epoch: | 334.5417° |
| orbit number at epoch: | 45764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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