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 29507U 06046C 23085.80403990 .00004619 00000-0 33710-3 0 9997
2 29507 97.6980 119.4890 0043901 2.7103 357.4352 15.03414146897266
| Epoch (UTC): | 26 March 2023 19:17:49 |
| Eccentricity: | 0.0043901 |
| inclination: | 97.6980° |
| perigee height: | 526 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 119.4890° |
| argument of perigee: | 2.7103° |
| revolutions per day: | 15.03414146 |
| mean anomaly at epoch: | 357.4352° |
| orbit number at epoch: | 89726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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