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 26047.14311028 +.00000000 +00000-0 +10717-3 0 00002
2 00047 66.6657 11.8756 0224296 228.1460 130.0313 14.45170046 08
| Epoch (UTC): | 16 February 2026 03:26:04 |
| Eccentricity: | 0.0224296 |
| inclination: | 66.6657° |
| perigee height: | 582 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 11.8756° |
| argument of perigee: | 228.1460° |
| revolutions per day: | 14.45170046 |
| mean anomaly at epoch: | 130.0313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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