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 23159.53332462 .00002978 00000-0 21527-3 0 9993
2 29507 97.6862 192.8040 0045211 109.7124 250.8987 15.04008815908349
| Epoch (UTC): | 08 June 2023 12:47:59 |
| Eccentricity: | 0.0045211 |
| inclination: | 97.6862° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 192.8040° |
| argument of perigee: | 109.7124° |
| revolutions per day: | 15.04008815 |
| mean anomaly at epoch: | 250.8987° |
| orbit number at epoch: | 90834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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