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 63996U 26145.43119795 +.00000000 +00000-0 +94794-3 0 00009
2 63996 43.0009 284.4553 0000136 308.5196 51.5644 15.27597104 00
| Epoch (UTC): | 25 May 2026 10:20:55 |
| Eccentricity: | 0.0000136 |
| inclination: | 43.0009° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.4553° |
| argument of perigee: | 308.5196° |
| revolutions per day: | 15.27597104 |
| mean anomaly at epoch: | 51.5644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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