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 47230U 26145.62930352 +.00000000 +00000-0 -35312-3 0 00005
2 47230 82.4993 315.6820 0014197 241.2104 118.7550 12.42928932 03
| Epoch (UTC): | 25 May 2026 15:06:11 |
| Eccentricity: | 0.0014197 |
| inclination: | 82.4993° |
| perigee height: | 1483 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 315.6820° |
| argument of perigee: | 241.2104° |
| revolutions per day: | 12.42928932 |
| mean anomaly at epoch: | 118.7550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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