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 17997U 26039.80063303 +.00000000 +00000-0 +96860-3 0 00001
2 17997 63.2916 208.7310 0699651 105.6532 262.2809 14.08965758 03
| Epoch (UTC): | 08 February 2026 19:12:54 |
| Eccentricity: | 0.0699651 |
| inclination: | 63.2916° |
| perigee height: | 356 km |
| apogee height: | 1370 km |
| right ascension of ascending node: | 208.7310° |
| argument of perigee: | 105.6532° |
| revolutions per day: | 14.08965758 |
| mean anomaly at epoch: | 262.2809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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