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 39160U 26118.83936641 +.00000000 +00000-0 +77642-4 0 00000
2 39160 97.9124 174.1404 0001263 88.5040 271.6309 14.64953597 02
| Epoch (UTC): | 28 April 2026 20:08:41 |
| Eccentricity: | 0.0001263 |
| inclination: | 97.9124° |
| perigee height: | 676 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 174.1404° |
| argument of perigee: | 88.5040° |
| revolutions per day: | 14.64953597 |
| mean anomaly at epoch: | 271.6309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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