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 68310U 26145.29795822 +.00000000 +00000-0 +23936-2 0 00008
2 68310 97.2847 271.5316 0001046 109.3059 250.8319 15.75331545 07
| Epoch (UTC): | 25 May 2026 07:09:03 |
| Eccentricity: | 0.0001046 |
| inclination: | 97.2847° |
| perigee height: | 343 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 271.5316° |
| argument of perigee: | 109.3059° |
| revolutions per day: | 15.75331545 |
| mean anomaly at epoch: | 250.8319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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