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 39763U 26110.58565411 +.00000000 +00000-0 -19759-3 0 00001
2 39763 82.4445 144.9919 0020906 195.7359 164.3074 12.42978648 06
| Epoch (UTC): | 20 April 2026 14:03:20 |
| Eccentricity: | 0.0020906 |
| inclination: | 82.4445° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 144.9919° |
| argument of perigee: | 195.7359° |
| revolutions per day: | 12.42978648 |
| mean anomaly at epoch: | 164.3074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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