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 26150.88320647 +.00000000 +00000-0 +32082-3 0 00002
2 41338 30.9979 74.9264 0009051 262.6954 97.2658 15.20683651 03
| Epoch (UTC): | 30 May 2026 21:11:49 |
| Eccentricity: | 0.0009051 |
| inclination: | 30.9979° |
| perigee height: | 498 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 74.9264° |
| argument of perigee: | 262.6954° |
| revolutions per day: | 15.20683651 |
| mean anomaly at epoch: | 97.2658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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