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 26070.87259463 +.00000000 +00000-0 +11542-3 0 00006
2 41634 75.0014 103.1501 0008669 270.9273 89.0923 14.93236394 02
| Epoch (UTC): | 11 March 2026 20:56:32 |
| Eccentricity: | 0.0008669 |
| inclination: | 75.0014° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 103.1501° |
| argument of perigee: | 270.9273° |
| revolutions per day: | 14.93236394 |
| mean anomaly at epoch: | 89.0923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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