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 47749U 26145.66668980 +.00000000 +00000-0 +91691-2 0 00009
2 47749 53.1547 186.4262 0001124 75.2393 60.5061 15.63728702 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.1547° |
| perigee height: | 376 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 186.4262° |
| argument of perigee: | 75.2393° |
| revolutions per day: | 15.63728702 |
| mean anomaly at epoch: | 60.5061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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