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 26020.27104414 +.00000000 +00000-0 +14910-3 0 00007
2 17528 97.4017 31.3487 0144829 165.3849 195.1606 14.54394678 02
| Epoch (UTC): | 20 January 2026 06:30:18 |
| Eccentricity: | 0.0144829 |
| inclination: | 97.4017° |
| perigee height: | 609 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 31.3487° |
| argument of perigee: | 165.3849° |
| revolutions per day: | 14.54394678 |
| mean anomaly at epoch: | 195.1606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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