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 15331U 26106.69024181 +.00000000 +00000-0 +52625-3 0 00005
2 15331 82.5091 354.5653 0005741 134.7076 225.4671 16.00426291 04
| Epoch (UTC): | 16 April 2026 16:33:56 |
| Eccentricity: | 0.0005741 |
| inclination: | 82.5091° |
| perigee height: | 269 km |
| apogee height: | 277 km |
| right ascension of ascending node: | 354.5653° |
| argument of perigee: | 134.7076° |
| revolutions per day: | 16.00426291 |
| mean anomaly at epoch: | 225.4671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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