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 15100U 26042.29526909 +.00000000 +00000-0 +19564-4 0 00005
2 15100 82.5332 145.3147 0013181 111.0642 249.1929 13.84551861 04
| Epoch (UTC): | 11 February 2026 07:05:11 |
| Eccentricity: | 0.0013181 |
| inclination: | 82.5332° |
| perigee height: | 938 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 145.3147° |
| argument of perigee: | 111.0642° |
| revolutions per day: | 13.84551861 |
| mean anomaly at epoch: | 249.1929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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