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 63689U 26145.60198355 +.00000000 +00000-0 +91039-4 0 00006
2 63689 86.5027 320.6713 0001400 83.4186 276.7107 13.24408047 02
| Epoch (UTC): | 25 May 2026 14:26:51 |
| Eccentricity: | 0.0001400 |
| inclination: | 86.5027° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.6713° |
| argument of perigee: | 83.4186° |
| revolutions per day: | 13.24408047 |
| mean anomaly at epoch: | 276.7107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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