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 47278U 26145.11543190 +.00000000 +00000-0 +10234-2 0 00005
2 47278 87.8952 355.2619 0001772 84.5375 275.5956 13.12441423 03
| Epoch (UTC): | 25 May 2026 02:46:13 |
| Eccentricity: | 0.0001772 |
| inclination: | 87.8952° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2619° |
| argument of perigee: | 84.5375° |
| revolutions per day: | 13.12441423 |
| mean anomaly at epoch: | 275.5956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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