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 26159.81218169 +.00000000 +00000-0 +42969-3 0 00001
2 39761 82.4445 113.9766 0021243 96.0955 264.2546 12.42878404 03
| Epoch (UTC): | 08 June 2026 19:29:32 |
| Eccentricity: | 0.0021243 |
| inclination: | 82.4445° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 113.9766° |
| argument of perigee: | 96.0955° |
| revolutions per day: | 12.42878404 |
| mean anomaly at epoch: | 264.2546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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