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 is defined by the following mean orbital elements,
1 47894U 26145.37755567 +.00000000 +00000-0 +92902-3 0 00003
2 47894 53.1518 271.3876 0001767 112.1820 247.9369 15.32146647 06
| Epoch (UTC): | 25 May 2026 09:03:40 |
| Eccentricity: | 0.0001767 |
| inclination: | 53.1518° |
| perigee height: | 468 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 271.3876° |
| argument of perigee: | 112.1820° |
| revolutions per day: | 15.32146647 |
| mean anomaly at epoch: | 247.9369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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