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 25567U 26106.60908728 +.00000000 +00000-0 +44100-4 0 00006
2 25567 82.9453 133.2930 0024318 278.8145 197.0054 13.72077139 08
| Epoch (UTC): | 16 April 2026 14:37:05 |
| Eccentricity: | 0.0024318 |
| inclination: | 82.9453° |
| perigee height: | 974 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 133.2930° |
| argument of perigee: | 278.8145° |
| revolutions per day: | 13.72077139 |
| mean anomaly at epoch: | 197.0054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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