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 00047U 26133.37071161 +.00000000 +00000-0 +51871-4 0 00001
2 00047 66.6624 140.1455 0216508 165.4262 195.3225 14.45279886 02
| Epoch (UTC): | 13 May 2026 08:53:49 |
| Eccentricity: | 0.0216508 |
| inclination: | 66.6624° |
| perigee height: | 587 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 140.1455° |
| argument of perigee: | 165.4262° |
| revolutions per day: | 14.45279886 |
| mean anomaly at epoch: | 195.3225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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