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 68849U 26145.58335647 +.00000000 +00000-0 +36686-3 0 00009
2 68849 97.2849 160.3054 0001506 96.2991 189.4236 15.49175014 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001506 |
| inclination: | 97.2849° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.3054° |
| argument of perigee: | 96.2991° |
| revolutions per day: | 15.49175014 |
| mean anomaly at epoch: | 189.4236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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