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 63120U 26145.49225192 +.00000000 +00000-0 +81454-3 0 00002
2 63120 43.0010 298.9619 0001583 264.2907 95.7764 15.27596490 09
| Epoch (UTC): | 25 May 2026 11:48:50 |
| Eccentricity: | 0.0001583 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 298.9619° |
| argument of perigee: | 264.2907° |
| revolutions per day: | 15.27596490 |
| mean anomaly at epoch: | 95.7764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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