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 34122U 93036KT 23275.86940417 .00009509 00000-0 22998-2 0 9996
2 34122 74.0445 202.0254 0106720 302.1641 114.1285 14.49732210770049
| Epoch (UTC): | 02 October 2023 20:51:56 |
| Eccentricity: | 0.0106720 |
| inclination: | 74.0445° |
| perigee height: | 651 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 202.0254° |
| argument of perigee: | 302.1641° |
| revolutions per day: | 14.49732210 |
| mean anomaly at epoch: | 114.1285° |
| orbit number at epoch: | 77004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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