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 63768U 26145.53937885 +.00000000 +00000-0 +70144-3 0 00008
2 63768 42.9985 330.9751 0001370 265.3991 94.6704 15.27599266 05
| Epoch (UTC): | 25 May 2026 12:56:42 |
| Eccentricity: | 0.0001370 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.9751° |
| argument of perigee: | 265.3991° |
| revolutions per day: | 15.27599266 |
| mean anomaly at epoch: | 94.6704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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