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 26020.95513618 +.00000000 +00000-0 +30979-3 0 00000
2 41634 75.0015 197.5745 0006740 26.1955 333.9573 14.93029145 02
| Epoch (UTC): | 20 January 2026 22:55:23 |
| Eccentricity: | 0.0006740 |
| inclination: | 75.0015° |
| perigee height: | 584 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 197.5745° |
| argument of perigee: | 26.1955° |
| revolutions per day: | 14.93029145 |
| mean anomaly at epoch: | 333.9573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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