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 68719U 26145.58335647 +.00000000 +00000-0 -41820-1 0 00000
2 68719 53.1601 36.9000 0000777 108.7554 332.3124 15.45196463 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000777 |
| inclination: | 53.1601° |
| perigee height: | 430 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 36.9000° |
| argument of perigee: | 108.7554° |
| revolutions per day: | 15.45196463 |
| mean anomaly at epoch: | 332.3124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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