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 39151U 13018B 22176.82210314 .00000900 00000-0 12308-3 0 9997
2 39151 97.9920 282.4557 0015887 224.5162 135.4774 14.80956737494919
Epoch (UTC): | 25 June 2022 19:43:49 |
Eccentricity: | 0.0015887 |
inclination: | 97.9920° |
perigee height: | 615 km |
apogee height: | 637 km |
right ascension of ascending node: | 282.4557° |
argument of perigee: | 224.5162° |
revolutions per day: | 14.80956737 |
mean anomaly at epoch: | 135.4774° |
orbit number at epoch: | 49491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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