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 63860U 26145.59944708 +.00000000 +00000-0 +46546-3 0 00008
2 63860 42.9994 3.6092 0000954 255.5126 104.5620 15.27596493 05
| Epoch (UTC): | 25 May 2026 14:23:12 |
| Eccentricity: | 0.0000954 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.6092° |
| argument of perigee: | 255.5126° |
| revolutions per day: | 15.27596493 |
| mean anomaly at epoch: | 104.5620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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