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 39153U 13018D 25139.13129095 .00005090 00000-0 48757-3 0 9992
2 39153 98.1165 278.9076 0012580 16.3194 343.8428 14.93581761652259
| Epoch (UTC): | 19 May 2025 03:09:03 |
| Eccentricity: | 0.0012580 |
| inclination: | 98.1165° |
| perigee height: | 578 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 278.9076° |
| argument of perigee: | 16.3194° |
| revolutions per day: | 14.93581761 |
| mean anomaly at epoch: | 343.8428° |
| orbit number at epoch: | 65225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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