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 63199U 26145.33060007 +.00000000 +00000-0 +59530-3 0 00003
2 63199 43.0006 12.4714 0001330 272.5287 87.5412 15.27574597 01
| Epoch (UTC): | 25 May 2026 07:56:03 |
| Eccentricity: | 0.0001330 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.4714° |
| argument of perigee: | 272.5287° |
| revolutions per day: | 15.27574597 |
| mean anomaly at epoch: | 87.5412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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