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 58U 60013A 25174.10644968 .00000098 00000-0 20529-4 0 9999
2 58 28.3248 161.7423 0164933 114.4363 247.3483 13.46412609186174
Epoch (UTC): | 23 June 2025 02:33:17 |
Eccentricity: | 0.0164933 |
inclination: | 28.3248° |
perigee height: | 962 km |
apogee height: | 1208 km |
right ascension of ascending node: | 161.7423° |
argument of perigee: | 114.4363° |
revolutions per day: | 13.46412609 |
mean anomaly at epoch: | 247.3483° |
orbit number at epoch: | 18617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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