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 63669U 26145.46338464 +.00000000 +00000-0 +12725-2 0 00008
2 63669 42.9976 175.8925 0000586 259.9849 100.0953 15.70855855 08
| Epoch (UTC): | 25 May 2026 11:07:16 |
| Eccentricity: | 0.0000586 |
| inclination: | 42.9976° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 175.8925° |
| argument of perigee: | 259.9849° |
| revolutions per day: | 15.70855855 |
| mean anomaly at epoch: | 100.0953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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