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 26150.48275353 +.00000000 +00000-0 +11013-2 0 00004
2 41340 30.9857 207.8812 0002421 158.6606 201.4154 15.84355645 08
| Epoch (UTC): | 30 May 2026 11:35:09 |
| Eccentricity: | 0.0002421 |
| inclination: | 30.9857° |
| perigee height: | 317 km |
| apogee height: | 320 km |
| right ascension of ascending node: | 207.8812° |
| argument of perigee: | 158.6606° |
| revolutions per day: | 15.84355645 |
| mean anomaly at epoch: | 201.4154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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