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 37212U 10058A 23087.36060041 .00000053 00000-0 00000-0 0 9997
2 37212 63.4848 202.2879 6415636 268.3580 22.6606 2.00596641 90850
Epoch (UTC): | 28 March 2023 08:39:15 |
Eccentricity: | 0.6415636 |
inclination: | 63.4848° |
perigee height: | 3141 km |
apogee height: | 37217 km |
right ascension of ascending node: | 202.2879° |
argument of perigee: | 268.3580° |
revolutions per day: | 2.00596641 |
mean anomaly at epoch: | 22.6606° |
orbit number at epoch: | 9085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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