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 52447U 26145.61412640 +.00000000 +00000-0 +90050-3 0 00004
2 52447 97.5647 261.0845 0003221 166.4288 193.7069 15.85578007 02
| Epoch (UTC): | 25 May 2026 14:44:20 |
| Eccentricity: | 0.0003221 |
| inclination: | 97.5647° |
| perigee height: | 313 km |
| apogee height: | 317 km |
| right ascension of ascending node: | 261.0845° |
| argument of perigee: | 166.4288° |
| revolutions per day: | 15.85578007 |
| mean anomaly at epoch: | 193.7069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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