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 26145.64459409 +.00000000 +00000-0 +10263-2 0 00002
2 39761 82.4429 122.8506 0020898 125.6300 234.6729 12.42878094 03
| Epoch (UTC): | 25 May 2026 15:28:12 |
| Eccentricity: | 0.0020898 |
| inclination: | 82.4429° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 122.8506° |
| argument of perigee: | 125.6300° |
| revolutions per day: | 12.42878094 |
| mean anomaly at epoch: | 234.6729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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