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 63161U 26145.55283066 +.00000000 +00000-0 +47733-4 0 00001
2 63161 88.9691 303.1656 0016367 20.7376 339.4436 13.51003849 08
| Epoch (UTC): | 25 May 2026 13:16:04 |
| Eccentricity: | 0.0016367 |
| inclination: | 88.9691° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 303.1656° |
| argument of perigee: | 20.7376° |
| revolutions per day: | 13.51003849 |
| mean anomaly at epoch: | 339.4436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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