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 47517U 26145.15019021 +.00000000 +00000-0 +14350-2 0 00009
2 47517 97.2062 208.5546 0007143 221.2583 138.8148 15.84735532 06
| Epoch (UTC): | 25 May 2026 03:36:16 |
| Eccentricity: | 0.0007143 |
| inclination: | 97.2062° |
| perigee height: | 312 km |
| apogee height: | 322 km |
| right ascension of ascending node: | 208.5546° |
| argument of perigee: | 221.2583° |
| revolutions per day: | 15.84735532 |
| mean anomaly at epoch: | 138.8148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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