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 26067.99163197 +.00000000 +00000-0 +12445-3 0 00006
2 41634 75.0005 108.6015 0008665 277.0755 82.9448 14.93229437 05
| Epoch (UTC): | 08 March 2026 23:47:57 |
| Eccentricity: | 0.0008665 |
| inclination: | 75.0005° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 108.6015° |
| argument of perigee: | 277.0755° |
| revolutions per day: | 14.93229437 |
| mean anomaly at epoch: | 82.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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