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 63012U 26145.55626904 +.00000000 +00000-0 +21968-2 0 00008
2 63012 43.0002 91.9477 0001389 296.7507 63.3219 15.70977989 03
| Epoch (UTC): | 25 May 2026 13:21:01 |
| Eccentricity: | 0.0001389 |
| inclination: | 43.0002° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 91.9477° |
| argument of perigee: | 296.7507° |
| revolutions per day: | 15.70977989 |
| mean anomaly at epoch: | 63.3219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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