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 25338U 26071.64337619 +.00000000 +00000-0 +93084-4 0 00007
2 25338 98.5160 94.8475 0009054 270.2692 89.7451 14.27113938 08
| Epoch (UTC): | 12 March 2026 15:26:27 |
| Eccentricity: | 0.0009054 |
| inclination: | 98.5160° |
| perigee height: | 795 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 94.8475° |
| argument of perigee: | 270.2692° |
| revolutions per day: | 14.27113938 |
| mean anomaly at epoch: | 89.7451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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