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 39761U 26053.79658699 +.00000000 +00000-0 +14402-3 0 00008
2 39761 82.4492 180.3613 0018959 330.2397 29.7603 12.42873387 00
| Epoch (UTC): | 22 February 2026 19:07:05 |
| Eccentricity: | 0.0018959 |
| inclination: | 82.4492° |
| perigee height: | 1480 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 180.3613° |
| argument of perigee: | 330.2397° |
| revolutions per day: | 12.42873387 |
| mean anomaly at epoch: | 29.7603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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