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 17911U 26042.16499171 +.00000000 +00000-0 +48063-3 0 00008
2 17911 82.5079 306.6921 0007150 46.5628 313.6217 15.50502292 07
| Epoch (UTC): | 11 February 2026 03:57:35 |
| Eccentricity: | 0.0007150 |
| inclination: | 82.5079° |
| perigee height: | 410 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 306.6921° |
| argument of perigee: | 46.5628° |
| revolutions per day: | 15.50502292 |
| mean anomaly at epoch: | 313.6217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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