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 25117.39947690 .00001501 00000-0 23453-3 0 9999
2 00029 48.3778 199.3592 0023123 278.1369 81.6921 14.77920876480612
| Epoch (UTC): | 27 April 2025 09:35:14 |
| Eccentricity: | 0.0023123 |
| inclination: | 48.3778° |
| perigee height: | 619 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 199.3592° |
| argument of perigee: | 278.1369° |
| revolutions per day: | 14.77920876 |
| mean anomaly at epoch: | 81.6921° |
| orbit number at epoch: | 48061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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