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 26087.95336365 +.00000000 +00000-0 +13623-3 0 00004
2 03764 101.4036 91.5206 0050679 268.4521 145.9680 12.49860936 06
| Epoch (UTC): | 28 March 2026 22:52:50 |
| Eccentricity: | 0.0050679 |
| inclination: | 101.4036° |
| perigee height: | 1425 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 91.5206° |
| argument of perigee: | 268.4521° |
| revolutions per day: | 12.49860936 |
| mean anomaly at epoch: | 145.9680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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