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 26138.07475071 +.00000000 +00000-0 +00000-0 0 00003
2 25967 9.8420 27.3666 0002477 337.2056 235.2412 1.00268506 07
| Epoch (UTC): | 18 May 2026 01:47:38 |
| Eccentricity: | 0.0002477 |
| inclination: | 9.8420° |
| perigee height: | 35777 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 27.3666° |
| argument of perigee: | 337.2056° |
| revolutions per day: | 1.00268506 |
| mean anomaly at epoch: | 235.2412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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