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 12669U 81053Z 24358.11834378 .00004314 00000-0 27645-2 0 9996
2 12669 82.9990 228.7895 0076588 302.6175 181.3974 14.01696389189088
Epoch (UTC): | 23 December 2024 02:50:24 |
Eccentricity: | 0.0076588 |
inclination: | 82.9990° |
perigee height: | 832 km |
apogee height: | 943 km |
right ascension of ascending node: | 228.7895° |
argument of perigee: | 302.6175° |
revolutions per day: | 14.01696389 |
mean anomaly at epoch: | 181.3974° |
orbit number at epoch: | 18908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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