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 03891U 26133.53805769 +.00000000 +00000-0 +28732-4 0 00008
2 03891 99.6537 6.5217 0039226 337.6354 137.9755 13.42975650 05
| Epoch (UTC): | 13 May 2026 12:54:48 |
| Eccentricity: | 0.0039226 |
| inclination: | 99.6537° |
| perigee height: | 1069 km |
| apogee height: | 1128 km |
| right ascension of ascending node: | 6.5217° |
| argument of perigee: | 337.6354° |
| revolutions per day: | 13.42975650 |
| mean anomaly at epoch: | 137.9755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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