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 41634U 26019.27992323 +.00000000 +00000-0 +12217-3 0 00002
2 41634 75.0016 200.7430 0006680 30.7129 329.4449 14.93019926 06
| Epoch (UTC): | 19 January 2026 06:43:05 |
| Eccentricity: | 0.0006680 |
| inclination: | 75.0016° |
| perigee height: | 584 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 200.7430° |
| argument of perigee: | 30.7129° |
| revolutions per day: | 14.93019926 |
| mean anomaly at epoch: | 329.4449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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