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 41340U 26098.74105613 +.00000000 +00000-0 +91940-3 0 00003
2 41340 30.9890 216.8638 0006164 74.0765 286.0569 15.69583296 03
| Epoch (UTC): | 08 April 2026 17:47:07 |
| Eccentricity: | 0.0006164 |
| inclination: | 30.9890° |
| perigee height: | 356 km |
| apogee height: | 364 km |
| right ascension of ascending node: | 216.8638° |
| argument of perigee: | 74.0765° |
| revolutions per day: | 15.69583296 |
| mean anomaly at epoch: | 286.0569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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