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 08344U 26159.15697397 +.00000000 +00000-0 +61953-4 0 00000
2 08344 74.0542 201.3544 0021757 357.7120 2.3932 14.40641445 01
| Epoch (UTC): | 08 June 2026 03:46:02 |
| Eccentricity: | 0.0021757 |
| inclination: | 74.0542° |
| perigee height: | 741 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 201.3544° |
| argument of perigee: | 357.7120° |
| revolutions per day: | 14.40641445 |
| mean anomaly at epoch: | 2.3932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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