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 47292U 26145.31025066 +.00000000 +00000-0 -12044-2 0 00002
2 47292 87.8959 355.2102 0002037 78.4221 281.7136 13.12442579 02
| Epoch (UTC): | 25 May 2026 07:26:45 |
| Eccentricity: | 0.0002037 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2102° |
| argument of perigee: | 78.4221° |
| revolutions per day: | 13.12442579 |
| mean anomaly at epoch: | 281.7136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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