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 39761U 26106.28116325 +.00000000 +00000-0 -18934-3 0 00001
2 39761 82.4456 147.5084 0019343 210.5536 149.4419 12.42875556 05
| Epoch (UTC): | 16 April 2026 06:44:52 |
| Eccentricity: | 0.0019343 |
| inclination: | 82.4456° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 147.5084° |
| argument of perigee: | 210.5536° |
| revolutions per day: | 12.42875556 |
| mean anomaly at epoch: | 149.4419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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