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 41338U 26053.18123625 +.00000000 +00000-0 +32772-3 0 00000
2 41338 30.9994 355.3871 0009299 339.9686 20.0589 15.19494452 08
| Epoch (UTC): | 22 February 2026 04:20:58 |
| Eccentricity: | 0.0009299 |
| inclination: | 30.9994° |
| perigee height: | 501 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 355.3871° |
| argument of perigee: | 339.9686° |
| revolutions per day: | 15.19494452 |
| mean anomaly at epoch: | 20.0589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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