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 47289U 26145.52371352 +.00000000 +00000-0 -91778-3 0 00005
2 47289 87.8958 355.1745 0001808 86.4096 273.7239 13.12441582 01
| Epoch (UTC): | 25 May 2026 12:34:08 |
| Eccentricity: | 0.0001808 |
| inclination: | 87.8958° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1745° |
| argument of perigee: | 86.4096° |
| revolutions per day: | 13.12441582 |
| mean anomaly at epoch: | 273.7239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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