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 26069.53261374 +.00000000 +00000-0 +11781-3 0 00006
2 41634 75.0003 105.6857 0008673 273.7438 86.2759 14.93233117 06
| Epoch (UTC): | 10 March 2026 12:46:57 |
| Eccentricity: | 0.0008673 |
| inclination: | 75.0003° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 105.6857° |
| argument of perigee: | 273.7438° |
| revolutions per day: | 14.93233117 |
| mean anomaly at epoch: | 86.2759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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