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 26044.55681182 +.00000000 +00000-0 +15343-3 0 00007
2 17528 97.4026 52.8557 0145943 89.2893 272.5026 14.54435783 08
| Epoch (UTC): | 13 February 2026 13:21:48 |
| Eccentricity: | 0.0145943 |
| inclination: | 97.4026° |
| perigee height: | 608 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 52.8557° |
| argument of perigee: | 89.2893° |
| revolutions per day: | 14.54435783 |
| mean anomaly at epoch: | 272.5026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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