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 223U 61015BK 24252.30010739 .00000207 00000-0 22979-3 0 9999
2 223 66.8892 90.4605 0061958 64.0852 296.6594 13.88864606201448
| Epoch (UTC): | 08 September 2024 07:12:09 |
| Eccentricity: | 0.0061958 |
| inclination: | 66.8892° |
| perigee height: | 887 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 90.4605° |
| argument of perigee: | 64.0852° |
| revolutions per day: | 13.88864606 |
| mean anomaly at epoch: | 296.6594° |
| orbit number at epoch: | 20144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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