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 63681U 26145.50529466 +.00000000 +00000-0 +63834-3 0 00009
2 63681 42.9993 316.6014 0001221 272.2963 87.7749 15.27587388 06
| Epoch (UTC): | 25 May 2026 12:07:37 |
| Eccentricity: | 0.0001221 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.6014° |
| argument of perigee: | 272.2963° |
| revolutions per day: | 15.27587388 |
| mean anomaly at epoch: | 87.7749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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