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 00117U 26046.14522152 +.00000000 +00000-0 +63645-4 0 00000
2 00117 66.8132 302.6727 0075363 18.5180 341.8614 13.90176002 07
| Epoch (UTC): | 15 February 2026 03:29:07 |
| Eccentricity: | 0.0075363 |
| inclination: | 66.8132° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 302.6727° |
| argument of perigee: | 18.5180° |
| revolutions per day: | 13.90176002 |
| mean anomaly at epoch: | 341.8614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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