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 29U 60002B 23026.97009692 .00001152 00000-0 19949-3 0 9998
2 29 48.3792 127.4797 0023915 351.4855 8.5648 14.74954404359363
| Epoch (UTC): | 26 January 2023 23:16:56 |
| Eccentricity: | 0.0023915 |
| inclination: | 48.3792° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 127.4797° |
| argument of perigee: | 351.4855° |
| revolutions per day: | 14.74954404 |
| mean anomaly at epoch: | 8.5648° |
| orbit number at epoch: | 35936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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