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 15506U 26040.27643395 +.00000000 +00000-0 +80747-4 0 00001
2 15506 82.9183 108.7737 0035599 216.1111 208.5355 13.76504383 05
| Epoch (UTC): | 09 February 2026 06:38:03 |
| Eccentricity: | 0.0035599 |
| inclination: | 82.9183° |
| perigee height: | 950 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 108.7737° |
| argument of perigee: | 216.1111° |
| revolutions per day: | 13.76504383 |
| mean anomaly at epoch: | 208.5355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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