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 26037.05465242 +.00000000 +00000-0 +11976-2 0 00007
2 41340 30.9921 288.3565 0002050 60.7004 299.3852 15.57677481 08
| Epoch (UTC): | 06 February 2026 01:18:41 |
| Eccentricity: | 0.0002050 |
| inclination: | 30.9921° |
| perigee height: | 393 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 288.3565° |
| argument of perigee: | 60.7004° |
| revolutions per day: | 15.57677481 |
| mean anomaly at epoch: | 299.3852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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