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 25967U 26144.06016691 +.00000000 +00000-0 +00000-0 0 00008
2 25967 9.8403 27.3441 0002932 331.6274 241.4022 1.00267754 05
| Epoch (UTC): | 24 May 2026 01:26:38 |
| Eccentricity: | 0.0002932 |
| inclination: | 9.8403° |
| perigee height: | 35775 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 27.3441° |
| argument of perigee: | 331.6274° |
| revolutions per day: | 1.00267754 |
| mean anomaly at epoch: | 241.4022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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