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 23403U 94076H 24357.82860075 .00000207 00000-0 71526-3 0 9998
2 23403 65.2009 152.3924 5647533 140.3104 265.6118 4.27454781467589
| Epoch (UTC): | 22 December 2024 19:53:11 |
| Eccentricity: | 0.5647533 |
| inclination: | 65.2009° |
| perigee height: | 602 km |
| apogee height: | 18717 km |
| right ascension of ascending node: | 152.3924° |
| argument of perigee: | 140.3104° |
| revolutions per day: | 4.27454781 |
| mean anomaly at epoch: | 265.6118° |
| orbit number at epoch: | 46758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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