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 00020U 26017.66465632 +.00000000 +00000-0 +43448-3 0 00005
2 00020 33.3495 88.8538 1639418 326.6389 24.0621 11.61738616 05
| Epoch (UTC): | 17 January 2026 15:57:06 |
| Eccentricity: | 0.1639418 |
| inclination: | 33.3495° |
| perigee height: | 507 km |
| apogee height: | 3207 km |
| right ascension of ascending node: | 88.8538° |
| argument of perigee: | 326.6389° |
| revolutions per day: | 11.61738616 |
| mean anomaly at epoch: | 24.0621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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