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 39762U 26053.85350992 +.00000000 +00000-0 +48005-3 0 00007
2 39762 82.4538 181.9707 0019486 324.9285 35.0510 12.42874196 01
| Epoch (UTC): | 22 February 2026 20:29:03 |
| Eccentricity: | 0.0019486 |
| inclination: | 82.4538° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 181.9707° |
| argument of perigee: | 324.9285° |
| revolutions per day: | 12.42874196 |
| mean anomaly at epoch: | 35.0510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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