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 26048.31961317 +.00000000 +00000-0 +10217-3 0 00009
2 00047 66.6658 8.7140 0224254 227.3072 130.8957 14.45171202 02
| Epoch (UTC): | 17 February 2026 07:40:14 |
| Eccentricity: | 0.0224254 |
| inclination: | 66.6658° |
| perigee height: | 582 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 8.7140° |
| argument of perigee: | 227.3072° |
| revolutions per day: | 14.45171202 |
| mean anomaly at epoch: | 130.8957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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