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 68829U 26145.49292409 +.00000000 +00000-0 +15606-3 0 00004
2 68829 96.6463 64.0025 0017010 122.9341 237.3569 15.82140565 09
| Epoch (UTC): | 25 May 2026 11:49:48 |
| Eccentricity: | 0.0017010 |
| inclination: | 96.6463° |
| perigee height: | 313 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 64.0025° |
| argument of perigee: | 122.9341° |
| revolutions per day: | 15.82140565 |
| mean anomaly at epoch: | 237.3569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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