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 26044.22937977 +.00000000 +00000-0 +30809-3 0 00005
2 00115 48.1632 350.3614 0026670 58.8504 301.5025 14.97297649 00
| Epoch (UTC): | 13 February 2026 05:30:18 |
| Eccentricity: | 0.0026670 |
| inclination: | 48.1632° |
| perigee height: | 557 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 350.3614° |
| argument of perigee: | 58.8504° |
| revolutions per day: | 14.97297649 |
| mean anomaly at epoch: | 301.5025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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