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 26022.47263007 +.00000000 +00000-0 +19798-3 0 00004
2 17528 97.4020 33.2983 0144978 158.4501 202.2886 14.54400185 02
| Epoch (UTC): | 22 January 2026 11:20:35 |
| Eccentricity: | 0.0144978 |
| inclination: | 97.4020° |
| perigee height: | 609 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 33.2983° |
| argument of perigee: | 158.4501° |
| revolutions per day: | 14.54400185 |
| mean anomaly at epoch: | 202.2886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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