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 26039.16672182 +.00000000 +00000-0 +78242-4 0 00002
2 00117 66.8143 319.6840 0074789 23.5201 336.9268 13.90174926 07
| Epoch (UTC): | 08 February 2026 04:00:04 |
| Eccentricity: | 0.0074789 |
| inclination: | 66.8143° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 319.6840° |
| argument of perigee: | 23.5201° |
| revolutions per day: | 13.90174926 |
| mean anomaly at epoch: | 336.9268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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