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 26072.94955928 +.00000000 +00000-0 +11412-3 0 00001
2 41634 75.0012 99.2199 0008680 266.4973 93.5223 14.93241732 03
| Epoch (UTC): | 13 March 2026 22:47:21 |
| Eccentricity: | 0.0008680 |
| inclination: | 75.0012° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 99.2199° |
| argument of perigee: | 266.4973° |
| revolutions per day: | 14.93241732 |
| mean anomaly at epoch: | 93.5223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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