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 26049.35770367 +.00000000 +00000-0 +93082-4 0 00009
2 00047 66.6660 5.9244 0224205 226.5626 131.6636 14.45171942 05
| Epoch (UTC): | 18 February 2026 08:35:05 |
| Eccentricity: | 0.0224205 |
| inclination: | 66.6660° |
| perigee height: | 582 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 5.9244° |
| argument of perigee: | 226.5626° |
| revolutions per day: | 14.45171942 |
| mean anomaly at epoch: | 131.6636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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