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 40069U 26145.62073273 +.00000000 +00000-0 +11076-3 0 00008
2 40069 98.5104 122.1603 0006945 99.0687 261.1277 14.21454636 08
| Epoch (UTC): | 25 May 2026 14:53:51 |
| Eccentricity: | 0.0006945 |
| inclination: | 98.5104° |
| perigee height: | 815 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 122.1603° |
| argument of perigee: | 99.0687° |
| revolutions per day: | 14.21454636 |
| mean anomaly at epoch: | 261.1277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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