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 17528U 26037.60830493 +.00000000 +00000-0 +16515-3 0 00008
2 17528 97.4024 46.7018 0145817 111.0186 250.6681 14.54425722 05
| Epoch (UTC): | 06 February 2026 14:35:57 |
| Eccentricity: | 0.0145817 |
| inclination: | 97.4024° |
| perigee height: | 608 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 46.7018° |
| argument of perigee: | 111.0186° |
| revolutions per day: | 14.54425722 |
| mean anomaly at epoch: | 250.6681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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