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 00115U 26050.10164197 +.00000000 +00000-0 +26755-3 0 00000
2 00115 48.1633 321.5102 0026558 85.9820 274.4133 14.97342959 03
| Epoch (UTC): | 19 February 2026 02:26:21 |
| Eccentricity: | 0.0026558 |
| inclination: | 48.1633° |
| perigee height: | 557 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 321.5102° |
| argument of perigee: | 85.9820° |
| revolutions per day: | 14.97342959 |
| mean anomaly at epoch: | 274.4133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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