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 47276U 26145.31872056 +.00000000 +00000-0 -34953-3 0 00007
2 47276 87.8961 355.1996 0001682 85.6192 274.5129 13.12442919 09
| Epoch (UTC): | 25 May 2026 07:38:57 |
| Eccentricity: | 0.0001682 |
| inclination: | 87.8961° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1996° |
| argument of perigee: | 85.6192° |
| revolutions per day: | 13.12442919 |
| mean anomaly at epoch: | 274.5129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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