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 41384U 26062.80677522 +.00000000 +00000-0 +00000-0 0 00006
2 41384 5.0828 99.2860 0019194 187.9817 197.1440 1.00270927 08
| Epoch (UTC): | 03 March 2026 19:21:45 |
| Eccentricity: | 0.0019194 |
| inclination: | 5.0828° |
| perigee height: | 35706 km |
| apogee height: | 35868 km |
| right ascension of ascending node: | 99.2860° |
| argument of perigee: | 187.9817° |
| revolutions per day: | 1.00270927 |
| mean anomaly at epoch: | 197.1440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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