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 03764U 26133.44188514 +.00000000 +00000-0 +11496-4 0 00008
2 03764 101.4024 134.9511 0051121 179.4989 342.1315 12.49861440 03
| Epoch (UTC): | 13 May 2026 10:36:18 |
| Eccentricity: | 0.0051121 |
| inclination: | 101.4024° |
| perigee height: | 1425 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 134.9511° |
| argument of perigee: | 179.4989° |
| revolutions per day: | 12.49861440 |
| mean anomaly at epoch: | 342.1315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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