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 39492U 26032.50133470 +.00000000 +00000-0 +19360-3 0 00008
2 39492 82.4133 42.2795 0017519 18.5331 341.6525 14.95584297 03
| Epoch (UTC): | 01 February 2026 12:01:55 |
| Eccentricity: | 0.0017519 |
| inclination: | 82.4133° |
| perigee height: | 568 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 42.2795° |
| argument of perigee: | 18.5331° |
| revolutions per day: | 14.95584297 |
| mean anomaly at epoch: | 341.6525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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