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 00029U 60002B 25197.91620941 .00000331 00000-0 74394-4 0 9993
2 00029 48.3770 177.1753 0022998 265.4559 94.3727 14.78056891492522
| Epoch (UTC): | 16 July 2025 21:59:20 |
| Eccentricity: | 0.0022998 |
| inclination: | 48.3770° |
| perigee height: | 619 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 177.1753° |
| argument of perigee: | 265.4559° |
| revolutions per day: | 14.78056891 |
| mean anomaly at epoch: | 94.3727° |
| orbit number at epoch: | 49252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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