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 26039.60343059 +.00000000 +00000-0 +14722-3 0 00005
2 17528 97.4026 48.4687 0145874 104.7864 256.9549 14.54428203 02
| Epoch (UTC): | 08 February 2026 14:28:56 |
| Eccentricity: | 0.0145874 |
| inclination: | 97.4026° |
| perigee height: | 608 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 48.4687° |
| argument of perigee: | 104.7864° |
| revolutions per day: | 14.54428203 |
| mean anomaly at epoch: | 256.9549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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