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 41884U 26106.94485664 +.00000000 +00000-0 +22068-3 0 00000
2 41884 34.9577 305.3004 0008234 296.1332 63.8544 15.54033560 02
| Epoch (UTC): | 16 April 2026 22:40:35 |
| Eccentricity: | 0.0008234 |
| inclination: | 34.9577° |
| perigee height: | 399 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 305.3004° |
| argument of perigee: | 296.1332° |
| revolutions per day: | 15.54033560 |
| mean anomaly at epoch: | 63.8544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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