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 07530U 74089B 25172.28541208 -.00000029 00000-0 10591-3 0 9991
2 07530 101.9927 176.6740 0012638 99.6170 272.3047 12.53689707315292
| Epoch (UTC): | 21 June 2025 06:50:59 |
| Eccentricity: | 0.0012638 |
| inclination: | 101.9927° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 176.6740° |
| argument of perigee: | 99.6170° |
| revolutions per day: | 12.53689707 |
| mean anomaly at epoch: | 272.3047° |
| orbit number at epoch: | 31529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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