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 59588U 26041.84481737 +.00000000 +00000-0 +15162-1 0 00009
2 59588 97.2203 348.9925 0045946 159.1023 201.2031 13.88488318 00
| Epoch (UTC): | 10 February 2026 20:16:32 |
| Eccentricity: | 0.0045946 |
| inclination: | 97.2203° |
| perigee height: | 900 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 348.9925° |
| argument of perigee: | 159.1023° |
| revolutions per day: | 13.88488318 |
| mean anomaly at epoch: | 201.2031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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