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 44786U 26145.62204541 +.00000000 +00000-0 +14201-3 0 00005
2 44786 88.9123 222.6512 0025228 211.7666 148.1968 13.55999921 00
| Epoch (UTC): | 25 May 2026 14:55:44 |
| Eccentricity: | 0.0025228 |
| inclination: | 88.9123° |
| perigee height: | 1032 km |
| apogee height: | 1069 km |
| right ascension of ascending node: | 222.6512° |
| argument of perigee: | 211.7666° |
| revolutions per day: | 13.55999921 |
| mean anomaly at epoch: | 148.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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