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 63123U 26145.43073249 +.00000000 +00000-0 +82330-3 0 00007
2 63123 42.9978 299.3624 0001532 282.9077 77.1604 15.27612078 01
| Epoch (UTC): | 25 May 2026 10:20:15 |
| Eccentricity: | 0.0001532 |
| inclination: | 42.9978° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 299.3624° |
| argument of perigee: | 282.9077° |
| revolutions per day: | 15.27612078 |
| mean anomaly at epoch: | 77.1604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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