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 26031.92445757 +.00000000 +00000-0 +12126-3 0 00003
2 03764 101.4017 38.0373 0051213 17.8445 43.5211 12.49860269 04
| Epoch (UTC): | 31 January 2026 22:11:13 |
| Eccentricity: | 0.0051213 |
| inclination: | 101.4017° |
| perigee height: | 1425 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 38.0373° |
| argument of perigee: | 17.8445° |
| revolutions per day: | 12.49860269 |
| mean anomaly at epoch: | 43.5211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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