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 26067.18764013 +.00000000 +00000-0 +13701-3 0 00007
2 41634 75.0005 110.1228 0008651 278.7810 81.2399 14.93227779 08
| Epoch (UTC): | 08 March 2026 04:30:12 |
| Eccentricity: | 0.0008651 |
| inclination: | 75.0005° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 110.1228° |
| argument of perigee: | 278.7810° |
| revolutions per day: | 14.93227779 |
| mean anomaly at epoch: | 81.2399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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