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 26103.90488119 +.00000000 +00000-0 -24097-3 0 00009
2 39763 82.4471 149.1767 0020648 210.4707 149.5174 12.42978116 04
| Epoch (UTC): | 13 April 2026 21:43:01 |
| Eccentricity: | 0.0020648 |
| inclination: | 82.4471° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 149.1767° |
| argument of perigee: | 210.4707° |
| revolutions per day: | 12.42978116 |
| mean anomaly at epoch: | 149.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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