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 26099.15261286 +.00000000 +00000-0 +25340-3 0 00006
2 41338 30.9982 54.1754 0008324 93.4983 266.6610 15.20196621 01
| Epoch (UTC): | 09 April 2026 03:39:45 |
| Eccentricity: | 0.0008324 |
| inclination: | 30.9982° |
| perigee height: | 500 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 54.1754° |
| argument of perigee: | 93.4983° |
| revolutions per day: | 15.20196621 |
| mean anomaly at epoch: | 266.6610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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