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 17295U 26020.67352575 +.00000000 +00000-0 +11756-2 0 00009
2 17295 82.4817 249.5673 0001972 40.8751 319.2667 15.85958552 03
| Epoch (UTC): | 20 January 2026 16:09:52 |
| Eccentricity: | 0.0001972 |
| inclination: | 82.4817° |
| perigee height: | 312 km |
| apogee height: | 315 km |
| right ascension of ascending node: | 249.5673° |
| argument of perigee: | 40.8751° |
| revolutions per day: | 15.85958552 |
| mean anomaly at epoch: | 319.2667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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