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 39679U 14021B 25118.14469545 .00023333 00000-0 64439-3 0 9990
2 39679 51.6086 65.5586 0116433 40.9662 319.9994 15.30350520608149
| Epoch (UTC): | 28 April 2025 03:28:21 |
| Eccentricity: | 0.0116433 |
| inclination: | 51.6086° |
| perigee height: | 395 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 65.5586° |
| argument of perigee: | 40.9662° |
| revolutions per day: | 15.30350520 |
| mean anomaly at epoch: | 319.9994° |
| orbit number at epoch: | 60814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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